Bot releases are visible (Hide)
Published by DzikuVx over 2 years ago
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
The I2C PCA9685 servo driver is no longer supported as obsolete and not widely adopted. All PCA9685 setups are advised to upgrade to SBUS output and SBUS to PWM
decoders
The align_acc
and align_gyro
settings are removed. Gyro/Acc orientation should always be set with align_board_yaw
The NAV_GPS_GLITCH_DETECTION
was removed as not suitable for modern aircraft. There is no user action required
INAV 5 removed the support for the following MSP frames:
MSP_IDENT
MSP_PID
MSP_PID_CONTROLLER
MSP_BF_CONFIG
MSP_BF_BUILD_INFO
MSP_SET_PID_CONTROLLER
MSP_SET_PID
MSP_SET_BF_CONFIG
MSP_CF_SERIAL_CONFIG
MSP_SET_CF_SERIAL_CONFIG
No user action is required in the case of the INAV Configurator or mwptools (mwp etc.). In the case of 3rd party INAV configuration apps, this change might break the compatibility if the app was using any of those frames. SpeedyBee
developers have been notified, other apps have to adjust accordingly.
In order to help mitigate the "randomly changed settings" bug, strict MSP payload length checking has been implemented. Fixed size MSP frames that do not specify the correct payload size will be rejected. The INAV Configurator and mwptools (mwp etc.) are compliant. In the case of 3rd party INAV configuration / mission planning / monitoring apps, this change might break interoperability if the app was not correctly setting the payload size. SpeedyBee
developers have been notified, other apps may have to adjust accordingly.
Please follow the instructions on this page.
INAV allows changing the function assignment of ALL PWM outputs. Bear in mind, that it's not resource mapping! This function allows assigning all outputs as motors or all outputs as servos. It's driven by CLI output_mode
setting
AUTO
assigns outputs according to the default mappingSERVOS
assigns all outputs to servosMOTORS
assigns all outputs to motorsUpdates landing detection for multirotor and add detection for fixed-wing. Detects when flying and activates landing detection from that point. Multirotor detection was added for non-autonomous landing as well as RTH. Fixed-wing detection is based on velocity, axis rates, and finally absolute movement in roll and pitch (so it probably wouldn't work if stuck in a tree being blown around by the wind). For details see https://github.com/iNavFlight/inav/pull/7270
LED hue can be updated with an RC channel. For example, CLI led 7 8,10::H:6
will adjust hue of LED number 7 based on RC channel 6. For details see https://github.com/iNavFlight/inav/pull/7618
This feature allows to arm of INAV aircraft on a boat or any other moving vehicle, as it allows to use of stored gyro calibration value instead of calibrating on every boot.
init_gyro_cal
If defined to OFF, it will ignore the gyroscope calibration done at each startup. Instead, the gyroscope's last calibration from when you calibrated will be used. It also means you don't have to keep the UAV stationary during a startup.gyro_zero_x
gyro X calibration storedgyro_zero_y
gyro Y calibration storedgyro_zero_z
gyro Z calibration storedProvides an option to force mission waypoint altitude to be achieved before moving on to the next waypoint. If the set altitude hasn't been achieved when the craft arrives at the waypoint it will hold and adjust the altitude as required with a target margin of 100cm. Planes use a spiral loiter whilst changing altitude. The option is set for the whole mission and applicable to basic and timed hold waypoints. For details see https://github.com/iNavFlight/inav/pull/7644
INAV will now use the SQRT
controller for Altitude Control on Multirotors. No extra pilot action required. For details see https://github.com/iNavFlight/inav/pull/7845
Adds the vtx_smartaudio_stopbits
setting that when set to 1
fixes the TBS Sixty9 SmartAudio 2.1 issues.
Adds following value as Logic Conditions Operands:
AGL_STATUS
boolean 1
when AGL can be trusted, 0
when AGL estimate can not be trustedAGL
integer Above The Groud Altitude in cm
RANGEFINDER_RAW
integer raw distance provided by the rangefinder in cm
To use the Matek 1G3SE with IRC Tramp. You will need to enter the CLI command set vtx_frequency_group = FREQUENCYGROUP_1G3
. You must also make sure that the initial VTx settings in the configuration tab are in a valid range. They are:
vtx_band
1 or 2vtx_channel
between 1 and 9The default VTx band has been changed from 4 to 1. If you are updating, please check that the band is still correct for your setup.
For details see https://github.com/iNavFlight/inav/pull/7949
KAKUTEH7
, MAMBAF722_2022A
and MAMBAH743
have now 4 motor and 4 servo outputs by default. To enable X8
mode, CLI set output_mode=MOTORS
command has to be used.
Name | Values |
---|---|
debug_modes | New: LANDING
|
servo_protocol | Removed: SERVO_DRIVER
|
Name | Description |
---|---|
ground_test_mode | For developer ground test use. Disables motors, sets heading status = Trusted on FW. Default: FALSE |
gyro_zero_x | Calculated gyro zero calibration of axis X Values: -32768 - 32767 Default: 0 |
gyro_zero_y | Calculated gyro zero calibration of axis Y Values: -32768 - 32767 Default: 0 |
gyro_zero_z | Calculated gyro zero calibration of axis Z Values: -32768 - 32767 Default: 0 |
init_gyro_cal | If defined to 'OFF', it will ignore the gyroscope calibration done at each startup. Instead, the gyroscope last calibration from when you calibrated will be used. It also means you don't have to keep the UAV stationary during a startup. Default: TRUE |
ins_gravity_cmss | Calculated 1G of Acc axis Z to use in INS Values: 0 - 2000 Default: 0.0 |
nav_fw_auto_disarm_delay | Delay before plane disarms when nav_disarm_on_landing is set (ms) Values: 100 - 10000 Default: 2000 |
nav_wp_enforce_altitude | Forces craft to achieve the set WP altitude as well as position before moving to next WP. Position is held and altitude adjusted as required before moving on. Default: FALSE |
osd_mah_used_precision | Number of digits used to display mAh used. Values: 4 - 6 Default: 4 |
osd_switch_indicator_one_channnel | RC Channel to use for OSD switch indicator 1. Default: 5 |
osd_switch_indicator_one_name | Character to use for OSD switch incicator 1. Values: 0 - 5 Default: GEAR |
osd_switch_indicator_three_channnel | RC Channel to use for OSD switch indicator 3. Default: 5 |
osd_switch_indicator_three_name | Character to use for OSD switch incicator 3. Values: 0 - 5 Default: LIGT |
osd_switch_indicator_two_channnel | RC Channel to use for OSD switch indicator 2. Default: 5 |
osd_switch_indicator_two_name | Character to use for OSD switch incicator 2. Values: 0 - 5 Default: CAM |
osd_switch_indicator_zero_channnel | RC Channel to use for OSD switch indicator 0. Default: 5 |
osd_switch_indicator_zero_name | Character to use for OSD switch incicator 0. Values: 0 - 5 Default: FLAP |
osd_switch_indicators_align_left | Align text to left of switch indicators Default: TRUE |
osd_system_msg_display_time | System message display cycle time for multiple messages (milliseconds). Values: 500 - 5000 Default: 1000 |
output_mode | Output function assignment mode. AUTO assigns outputs according to the default mapping, SERVOS assigns all outputs to servos, MOTORS assigns all outputs to motors Default: AUTO |
vtx_frequency_group | VTx Frequency group to use. Frequency groups: FREQUENCYGROUP_5G8: 5.8GHz, FREQUENCYGROUP_2G4: 2.4GHz, FREQUENCYGROUP_1G3: 1.3GHz. Values: 0 - 2 Default: FREQUENCYGROUP_5G8 |
vtx_smartaudio_stopbits | Set stopbit count for serial (TBS Sixty9 SmartAudio 2.1 require value of 1 bit) Values: 1 - 2 Default: 2 |
vtx_softserial_shortstop | Enable the 3x shorter stopbit on softserial. Need for some IRC Tramp VTXes. Default: FALSE |
Name | Description |
---|---|
align_acc | Use align_board_yaw
|
align_gyro | Use align_board_yaw
|
ninja
as build manager by @stronnag in https://github.com/iNavFlight/inav/pull/7942
The full list of changes is available here
The full list of INAV Configurator changes is available here
Published by DzikuVx over 2 years ago
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
This release is fully supported only with INAV Configurator 4.1. When an older version of Configurator is used, the OSD tab will not work!
diff
of the current configurationdiff
outputFULL CHIP ERASE
diff
with the CLI tabPlease follow the instructions on this page.
The full list of changes is available here
Published by DzikuVx over 2 years ago
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
This release is fully supported only with INAV Configurator 4.1. When an older version of Configurator is used, the OSD tab will not work!
diff
of the current configurationdiff
outputFULL CHIP ERASE
diff
with the CLI tabPlease follow the instructions on this page.
The full list of changes is available here
Published by DzikuVx almost 3 years ago
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
If you use a PPM receiver, these are no longer supported by iNav. We recommend that you use serial based receivers.
Due to the storage space on these flight controllers. Features have started to be dropped. See PR #7297 for details
A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
If you are using the INAV LUA script and Crossfire, you should update to the latest INAV LUA script.
Please follow the instructions on this page.
With INAV 4.0 there are a couple of important changes in how gyro and D-term are filtered. They mostly affect Multirotor pilots.
INAV 4.0 comes with the full support of all H7 boards compatible with MATEKH743 target. This includes the SD Card and MSC mode support. Bear in mind, CAN and UAVCAN are still not supported by INAV and currently, there are no plans to implement them.
Blackbox now always logs the Control Derivative and Feed Forward components, as well as rate target in degrees-per-seconds.
The latest INAV Blackbox Explorer is required to fully use those features.
New command blackbox
allows setting which Blackbox fields are recorded to conserve space and bandwidth. Possible fields are:
Usage
blackbox
currently enabled Blackbox fieldsblackbox list
all available fieldsblackbox -MOTORS
disable MOTORS loggingblackbox MOTOR
enable MOTORS loggingINAV 4.0 adds a port of the EmuFlight Rate Dynamics system. It modifies stick input to change the flight feeling. To find out more refer to:
Below are some presets you might want to try
set rate_dynamics_center_sensitivity = 100
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 0
set rate_dynamics_end_sensitivity = 100
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 0
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 20
set rate_dynamics_center_weight = 85
set rate_dynamics_end_sensitivity = 90
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 50
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 35
set rate_dynamics_end_sensitivity = 130
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 35
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 35
set rate_dynamics_end_sensitivity = 130
set rate_dynamics_end_correction = 30
set rate_dynamics_end_weight = 35
set rate_dynamics_center_sensitivity = 130
set rate_dynamics_center_correction = 35
set rate_dynamics_center_weight = 30
set rate_dynamics_end_sensitivity = 115
set rate_dynamics_end_correction = 20
set rate_dynamics_end_weight = 10
Multiple missions may be uploaded to the flight controller and a mission selected for execution by OSD, Stick Command or Mission Planner. Multi-Mission is supported by the inav Configurator and mwp mission planners.
The maximum number of WPs is now 120.
INAV 4.0 adds the capability to generate an "on the fly" mission while flying using aircraft positions.
INAV 4.0 adds Fly-by-home waypoints. This is a waypoint whose location is set to the home position at arm time.
The soaring mode comes to iNav 4.0. The addition is great for people who fly gliders. The soaring mode adds a modifier that you can use to change how Course Hold, Cruise, or Position Hold (loiter) behave. When enabled, it disables altitude control and allows Angle mode to free float in pitch, allowing the plane to soar freely.
This change allows the climb phase of a climb first RTH to have two separate parts. This is useful for pilots who want to climb first, to clear potential obstacles. But, don't want to be wasting energy flying away from home. This allows you to set a first climb stage altitude. Once it meets or exceeds that altitude, the plane will turn to home and continue climbing to the RTH altitude. See the iNav Wiki for more information.
There were often autotunes in iNav 3.0 which resulted in too high P and I. Also, D was not tuned at all. New default PIDs, that will work reasonably on all sizes of planes (#1390) have been added. This should give good results with an autotune, which can then be fine tuned to your plane.
If you previously used the UK units in your OSD. You will now find that your units are set to Metric + MPH. This is the new name for the old UK units. There is also a new UK units set, that better represents transportation units used in the UK. Full details can be found in the pull release.
There is also a new units set aimed at General Aviation pilots. This set uses Knots, Feet, Nautical Miles, 100 Feet per Minute, and Celsius for their respective values.
The full list of changes is available here
You can get more suggestions following this link too.
Published by DzikuVx almost 3 years ago
Hello and welcome to INAV 4.0.0 Release Candidate 2!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
If you use a PPM receiver, these are no longer supported by iNav. We recommend that you use serial based receivers.
Due to the storage space on these flight controllers. Features have started to be dropped. See PR #7297 for details
A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
Please follow the instructions on this page.
With INAV 4.0 there are a couple of important changes in how gyro and D-term are filtered. They mostly affect Multirotor pilots.
INAV 4.0 comes with the full support of all H7 boards compatible with MATEKH743 target. This includes the SD Card and MSC mode support. Bear in mind, CAN and UAVCAN are still not supported by INAV and currently, there are no plans to implement them.
Blackbox now always logs the Control Derivative and Feed Forward components, as well as rate target in degrees-per-seconds.
The latest INAV Blackbox Explorer is required to fully use those features.
New command blackbox
allows setting which Blackbox fields are recorded to conserve space and bandwidth. Possible fields are:
Usage
blackbox
currently enabled Blackbox fieldsblackbox list
all available fieldsblackbox -MOTORS
disable MOTORS loggingblackbox MOTOR
enable MOTORS loggingINAV 4.0 adds a port of the EmuFlight Rate Dynamics system. It modifies stick input to change the flight feeling. To find out more refer to:
Below are some presets you might want to try
set rate_dynamics_center_sensitivity = 100
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 0
set rate_dynamics_end_sensitivity = 100
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 0
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 20
set rate_dynamics_center_weight = 85
set rate_dynamics_end_sensitivity = 90
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 50
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 35
set rate_dynamics_end_sensitivity = 130
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 35
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 35
set rate_dynamics_end_sensitivity = 130
set rate_dynamics_end_correction = 30
set rate_dynamics_end_weight = 35
set rate_dynamics_center_sensitivity = 130
set rate_dynamics_center_correction = 35
set rate_dynamics_center_weight = 30
set rate_dynamics_end_sensitivity = 115
set rate_dynamics_end_correction = 20
set rate_dynamics_end_weight = 10
Multiple missions may be uploaded to the flight controller and a mission selected for execution by OSD, Stick Command or Mission Planner. Multi-Mission is supported by the inav Configurator and mwp mission planners.
The maximum number of WPs is now 120.
Inav 4.0 adds the capability to generate an "on the fly" mission while flying using aircraft positions.
Inav 4.0 adds Fly-by-home waypoints. This is a way point whose location is set to the home position at arm time.
Soaring mode comes to iNav 4.0. The addition is great for people who fly gliders. Soaring mode adds a modifier that you can use to change how Course Hold, Cruise, or Position Hold (loiter) behave. When enabled, it disables altitude control and allows Angle mode to free float in pitch, allows the plane to soar freely.
This change allows the climb phase of a climb first RTH to have two separate parts. This is useful for pilots who want to climb first, to clear potential obstacles. But, don't want to be wasting energy flying away from home. This allows you to set a first climb stage altitude. Once it meets or exceeds that altitude, the plane will turn to home and continue climbing to the RTH altitude. See the iNav Wiki for more information.
There were often autotunes in iNav 3.0 which resulted in too high P and I. Also, D was not tuned at all. New default PIDs, that will work reasonably on all sizes of planes (#1390) have been added. This should give good results with an autotune, which can then be fine tuned to your plane.
If you previously used the UK units in your OSD. You will now find that your units are set to Metric + MPH. This is the new name for the old UK units. There is also a new UK units set, that better represents transportation units used in the UK. Full details can be found in the pull release.
There is also a new units set aimed at General Aviation pilots. This set uses Knots, Feet, Nautical Miles, 100 Feet per Minute, and Celsius for their respective values.
The full list of changes is available here
Published by DzikuVx almost 3 years ago
Hello and welcome to INAV 4.0.0 Release Candidate 1!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
If you use a PPM receiver, these are no longer supported by iNav. We recommend that you use serial based receivers.
Due to the storage space on these flight controllers. Features have started to be dropped. See PR #7297 for details
A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
Please follow the instructions on this page.
With INAV 4.0 there are a couple of important changes in how gyro and D-term are filtered. They mostly affect Multirotor pilots.
INAV 4.0 comes with the full support of all H7 boards compatible with MATEKH743 target. This includes the SD Card and MSC mode support. Bear in mind, CAN and UAVCAN are still not supported by INAV and currently, there are no plans to implement them.
Blackbox now always logs the Control Derivative and Feed Forward components, as well as rate target in degrees-per-seconds.
The latest INAV Blackbox Explorer is required to fully use those features.
New command blackbox
allows setting which Blackbox fields are recorded to conserve space and bandwidth. Possible fields are:
Usage
blackbox
currently enabled Blackbox fieldsblackbox list
all available fieldsblackbox -MOTORS
disable MOTORS loggingblackbox MOTOR
enable MOTORS loggingINAV 4.0 adds a port of the EmuFlight Rate Dynamics system. It modifies stick input to change the flight feeling. To find out more refer to:
Below are some presets you might want to try
set rate_dynamics_center_sensitivity = 100
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 0
set rate_dynamics_end_sensitivity = 100
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 0
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 20
set rate_dynamics_center_weight = 85
set rate_dynamics_end_sensitivity = 90
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 50
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 35
set rate_dynamics_end_sensitivity = 130
set rate_dynamics_end_correction = 10
set rate_dynamics_end_weight = 35
set rate_dynamics_center_sensitivity = 80
set rate_dynamics_center_correction = 10
set rate_dynamics_center_weight = 35
set rate_dynamics_end_sensitivity = 130
set rate_dynamics_end_correction = 30
set rate_dynamics_end_weight = 35
set rate_dynamics_center_sensitivity = 130
set rate_dynamics_center_correction = 35
set rate_dynamics_center_weight = 30
set rate_dynamics_end_sensitivity = 115
set rate_dynamics_end_correction = 20
set rate_dynamics_end_weight = 10
Multiple missions may be uploaded to the flight controller and a mission selected for execution by OSD, Stick Command or Mission Planner. Multi-Mission is supported by the inav Configurator and mwp mission planners.
The maximum number of WPs is now 120.
Inav 4.0 adds the capability to generate an "on the fly" mission while flying using aircraft positions.
Inav 4.0 adds Fly-by-home waypoints. This is a way point whose location is set to the home position at arm time.
Soaring mode comes to iNav 4.0. The addition is great for people who fly gliders. Soaring mode adds a modifier that you can use to change how Course Hold, Cruise, or Position Hold (loiter) behave. When enabled, it disables altitude control and allows Angle mode to free float in pitch, allows the plane to soar freely.
This change allows the climb phase of a climb first RTH to have two separate parts. This is useful for pilots who want to climb first, to clear potential obstacles. But, don't want to be wasting energy flying away from home. This allows you to set a first climb stage altitude. Once it meets or exceeds that altitude, the plane will turn to home and continue climbing to the RTH altitude. See the iNav Wiki for more information.
There were often autotunes in iNav 3.0 which resulted in too high P and I. Also, D was not tuned at all. New default PIDs, that will work reasonably on all sizes of planes (#1390) have been added. This should give good results with an autotune, which can then be fine tuned to your plane.
If you previously used the UK units in your OSD. You will now find that your units are set to Metric + MPH. This is the new name for the old UK units. There is also a new UK units set, that better represents transportation units used in the UK. Full details can be found in the pull release.
There is also a new units set aimed at General Aviation pilots. This set uses Knots, Feet, Nautical Miles, 100 Feet per Minute, and Celsius for their respective values.
The full list of changes is available here
Published by DzikuVx about 3 years ago
Hello and welcome to INAV 3.0.2 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
The OSD fonts have been improved (@Jettrel) and there are several new symbols. A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
dump
commandINAV 3.0.2
with Full Chip EraseAlternatively, flash 3.0.2
without Full Chip Erase - Not recommended
You can get more suggestions following this link too.
Published by DzikuVx over 3 years ago
Hello and welcome to INAV 3.0.1 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
The OSD fonts have been improved (@Jettrel) and there are several new symbols. A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
dump
commandINAV 3.0.1
with Full Chip EraseAlternatively, flash 3.0.1
without Full Chip Erase - Not recommended
This release supports Matek H743-WING, H743-Slim, and H743-Mini flight controllers. Targets are fully flyable, but not all features are yet working:
INAV Configurator 3.0.1 is required to flash H743 targets with Full Chip Erase.
We suggest NOT to do a full diff
or dump
upgrade. To get the best performance set up your aircraft from scratch. You can copy osd
, aux
, serial
, and mixer settings, as well as accelerometer and magnetometer calibration values from INAV 2.6, but other settings should be tuned again.
Please follow the instructions on this page.
Setting | Description |
---|---|
imu2 | Display the current status of the Secondary IMU |
imu2 fetch | Get calibration data from the Secondary IMU |
pid | Configure general purpose PID controllers. Refer to docs |
Setting | Description |
---|---|
blackbox_device | Default: target |
log_level | Default: ERROR |
nav_overrides_motor_stop | When set to OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect on NAV modes which take control of the throttle when combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV |
nav_rth_climb_first | New: ON_FW_SPIRAL
|
platform_type | Default: MULTIROTOR |
receiver_type | Default: target |
rssi_source | Default: AUTO |
Setting | Description |
---|---|
dji_speed_source | Sets the speed type displayed by the DJI OSD: GROUND, 3D, AIR Default: GROUND |
dshot_beeper_enabled | Whether using DShot motors as beepers is enabled Default: TRUE |
dshot_beeper_tone | Sets the DShot beeper tone Values: 1 - 5 Default: 1 |
fw_d_pitch | Fixed wing rate stabilisation D-gain for PITCH Default: 0 |
fw_d_roll | Fixed wing rate stabilisation D-gain for ROLL Default: 0 |
fw_d_yaw | Fixed wing rate stabilisation D-gain for YAW Default: 0 |
fw_level_pitch_trim | Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level Values: -10 - 10 Default: 0 |
fw_yaw_iterm_freeze_bank_angle | Yaw Iterm is frozen when bank angle is above this threshold [degrees]. This solves the problem of the rudder counteracting turns by partially disabling yaw stabilization when making banked turns. Setting to 0 (the default) disables this feature. Only applies when autopilot is not active and TURN ASSIST is disabled. Values: 0 - 90 Default: 0 |
gyro_abg_alpha | Alpha factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 1 Default: 0 |
gyro_abg_boost | Boost factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 2 Default: 0.35 |
gyro_abg_half_life | Sample half-life for Gyro Alpha-Beta-Gamma filter Values: 0 - 10 Default: 0.5 |
gyro_anti_aliasing_lpf_hz | Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz Values: 0 - 255 Default: 250 |
gyro_anti_aliasing_lpf_type | Specifies the type of the software LPF of the gyro signals. Default: PT1 |
gyro_dyn_lpf_curve_expo | Expo value for the throttle-to-frequency mapping for Dynamic LPF Values: 1 - 10 Default: 5 |
gyro_dyn_lpf_max_hz | Maximum frequency of the gyro Dynamic LPF Values: 40 - 1000 Default: 500 |
gyro_dyn_lpf_min_hz | Minimum frequency of the gyro Dynamic LPF Values: 40 - 400 Default: 200 |
gyro_main_lpf_hz | Software based gyro main lowpass filter. Value is cutoff frequency (Hz) Values: 0 - 500 Default: 60 |
gyro_main_lpf_type | Defines the type of the main gyro LPF filter. Possible values: PT1 , BIQUAD . PT1 offers faster filter response while BIQUAD better attenuation. Default: BIQUAD |
gyro_use_dyn_lpf | Use Dynamic LPF instead of static gyro stage1 LPF. Dynamic Gyro LPF updates gyro LPF based on the throttle position. Default: FALSE |
imu2_align_pitch | Pitch alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_roll | Roll alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_yaw | Yaw alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_gain_acc_x | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_y | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_z | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_x | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_y | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_z | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_hardware | Selection of a Secondary IMU hardware type. NONE disables this functionality Default: NONE, values NONE , BNO055 , BNO055_SERIAL
|
imu2_radius_acc | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_radius_mag | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_use_for_osd_ahi | If set to ON, Secondary IMU data will be used for Analog OSD Artificial Horizon Default: FALSE |
imu2_use_for_osd_heading | If set to ON, Secondary IMU data will be used for Analog OSD heading Default: FALSE |
imu2_use_for_stabilized | If set to ON, Secondary IMU data will be used for Angle, Horizon and all other modes that control attitude (PosHold, WP, RTH) Default: FALSE |
mavlink_version | Version of MAVLink to use Values: 1 - 2 Default: 2 |
nav_land_maxalt_vspd | Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s] Values: 100 - 2000 Default: 200 |
nav_land_minalt_vspd | Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s] Values: 50 - 500 Default: 50 |
nav_max_altitude | Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled Values: 0 - 65000 Default: 0 |
nav_mc_wp_slowdown | When ON, NAV engine will slow down when switching to the next waypoint. This prioritizes turning over forward movement. When OFF, NAV engine will continue to the next waypoint and turn as it goes. Default: TRUE |
nav_rth_alt_control_override | If set to ON RTH altitude and CLIMB FIRST settings can be overridden during the RTH climb phase using full pitch or roll stick held for > 1 second. RTH altitude is reset to the current altitude using pitch down stick. RTH CLIMB FIRST is overridden using right roll stick so craft turns and heads directly to home (CLIMB FIRST override only works for fixed wing) Default: FALSE |
osd_pan_servo_index | Index of the pan servo to adjust osd home heading direction based on camera pan. Note that this feature does not work with continiously rotating servos. Values: 0 - 10 Default: 0 |
osd_pan_servo_pwm2centideg | Centidegrees of pan servo rotation us PWM signal. A servo with 180 degrees of rotation from 1000 to 2000 us PWM typically needs 18 for this setting. Change sign to inverse direction. Values: -36 - 36 Default: 0 |
osd_plus_code_short | Number of leading digits removed from plus code. Removing 2, 4 and 6 digits requires a reference location within, respectively, ~800km, ~40 km and ~2km to recover the original coordinates. Default: 0 |
osd_sidebar_height | Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD) Values: 0 - 5 Default: 3 |
osd_stats_min_voltage_unit | Display minimum voltage of the BATTERY or the average per CELL in the OSD stats. Default: BATTERY. Options BATTERY , CELL
|
osd_telemetry | To enable OSD telemetry for antenna tracker. Possible values are OFF , ON and TEST Default: OFF |
prearm_timeout | Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout. Values: 0 - 10000 Default: 10000 |
safehome_max_distance | In order for a safehome to be used, it must be less than this distance (in cm) from the arming point. Values: 0 - 65000 Default: 20000 |
safehome_usage_mode | Used to control when safehomes will be used. Possible values are OFF , RTH and RTH_FS . See Safehome documentation for more information. Default: RTH |
servo_autotrim_rotation_limit | Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using feature FW_AUTOTRIM . Values: 1 - 60 Default: 15 |
smith_predictor_delay | Expected delay of the gyro signal. In milliseconds Values: 0 - 8 Default: 0 |
smith_predictor_lpf_hz | Cutoff frequency for the Smith Predictor Low Pass Filter Values: 1 - 500 Default: 50 |
smith_predictor_strength | The strength factor of a Smith Predictor of PID measurement. In percents Values: 0 - 1 Default: 0.5 |
turtle_mode_power_factor | Turtle mode power factor Values: 0 - 100 Default: 55 |
vtx_smartaudio_early_akk_workaround | Enable workaround for early AKK SAudio-enabled VTX bug. Default: TRUE |
osd_rssi_dbm_alarm | RSSI in dBm alarm for Crossfire. Default: 0 |
nav_wp_load_on_boot | If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup. Default: OFF |
Setting | Description |
---|---|
gyro_sync | |
nav_landing_speed | replaced by nav_land_minalt_vspd and nav_land_maxalt_vspd
|
Old name | New name |
---|---|
gyro_lpf_hz | Replaced with gyro_main_lpf_hz
|
gyro_lpf_type | Replaced with gyro_main_lpf_type
|
gyro_stage2_lowpass_hz | Replaced with gyro_anti_aliasing_lpf_hz
|
gyro_stage2_lowpass_type | Replaced with gyro_anti_aliasing_lpf_type
|
mc_airmode_threshold | airmode_threshold |
mc_airmode_type | airmode_type |
osd_artificial_horizon_max_pitch | osd_ahi_max_pitch |
osd_artificial_horizon_reverse_roll | osd_ahi_reverse_roll |
INAV now has a "Turtle Mode".
Prior to inav 3.0, mission waypoint altitudes are relative the arming location. It is now possible to define waypoints with absolute (AMSL) altitude, making the mission independent of the arming location. See the inav wiki for details (WP paramater 3
)
The relative / absolute ground altitude of a LAND
waypoint may be set as WP paramater 2
(m). See the inav wiki for details.
Nothing to add. If DSHOT is enabled, DSHOT beeper will be used.
MAVLink is still only a downlink from UAV to the ground station, but now allows to use RC-Over-MAVLink
Prearm offers a two-stage arming process as an optional additional safety feature.
H7 is available in the source repository; target Hex files will be released as targets mature, probably in the future point releases.
You can now use the D-gain to improve the stabilization, especially on small and agile airplanes. Until we have a better understanding of how to tune this on a range of airplanes, the D-gain is set to zero by default and not tuned using autotune. Please report good performing tunes in https://github.com/iNavFlight/inav/issues/6709.
AUTOTUNE can now automatically set the correct rates for your airplane. The goal is to set rates that the airplane is capable of achieving with 80% control surface deflection so there is some room for the stabilization to work. This feature is controlled by CLI setting fw_autotune_rate_adjustment
. When set to AUTO
(the default), autotune automatically determines the rates and gains. When set to MAX
, rates will be automatically adjusted, but never above the starting values. This can be used to calm down a very agile plane, while still avoiding setting too high rates. When set to FIXED
, rates will not be adjusted. Note that setting too high rates can cause very bad flight behavior and potential crashes. Rate discovery is not possible in ANGLE mode so it is highly advised to do autotune in ACRO mode.
There is now the option to continuously trim the servos for straight and level flight. When enabled and flying straight and level, INAV records what servo output is required to maintain a constant attitude, and adjusts the servo midpoints accordingly. The servo midpoints are limited to the 1300-1700 range. After the first maiden flight, and after the first flight when significant changes have been made to the airplane, check the servo midpoints. If they are at or close to the end of this range mechanically adjust the control surfaces.
As part of gyro processing updates, the following changes were made:
gyro_sync
is gone, INAV no longer does a wait cycle trying to get the next set of data from the gyro.gyro_anti_aliasing_lpf_hz
). In normal circumstances, there is no need to change this settinggyro_lpf_hz
was renamed to gyro_main_lpf_hz
set smith_predictor_delay = 3
. More details about this feature will follow laterset gyro_abg_alpha = 0.25
or higher value. It requires a very clean gyro signal or might introduce oscillations on the high throttle. If the multirotor started to vibrate after enabling the Alpha-Beta-Gamma filter, you either have to improve the gyro filter strategy or disable the ABG filter. It works great on some builds and not so great or other. It's up to you to test.set gyro_use_dyn_lpf=ON
and set gyro_dyn_lpf_min_hz
and gyro_dyn_lpf_max_hz
. Dynamic LPF replaces gyro_main_lpf_hz
The EGNOS (GPS ground assistance) definitions have been updated to the latest values for all GNSS options. An invalid association with the availability of Galileo has been corrected.
New FCs rarely feature onboard compass, and most GPS+MAG default to CW270FLIP, so this is now the INAV default. If you use another value, check your setup after upgrading.
To more clearly state what they do and how they work. It's a subtle, but worth it to change for sure!
Users must upgrade OSD Fonts to Version 2 (or later).
Safehome does not now replace the arming location until it is needed. If you cancel RTH or recover from RX failsafe, the original arming location is restored as the home location. Under normal circumstances, "distance to home" will revert to range from the arming location.
Provides stick options to override configured RTH climb and/or turn behaviour. See the nav_rth_alt_control_override
setting description for details.
Modes names were changed to be more user friendly. When OSD OFF
is enabled, OSD will be turned off. When LED OFF
is enabled, LEDs will be turned off.
Yeap, now when nav_rth_climb_first
is set to ON_FW_SPIRAL
, Fixed Wing will keep litering and gaining altitude until it reaches desired altitude. Previously, it was climbing while flying straight in random direction
When nav_mc_wp_slowdown
is set to OFF
, Waypoint missions on Multirotors will be smoother as the NAV engine will not try to slow down before entering the waypoint and then accelerate towards the next waypoint. INAV will rather enter WP with normal speed, switch to the next waypoint and then adjust heading while flying.
The default behavior of the DJI OSD speed element was to display a ground speed. osd_speed_source
can be set to GROUND, AIR or 3D speed depending on the preference
fw_level_pitch_trim
setting. +5 fw_level_pitch_trim
means airplane nose should be raised 5 deg from levelAUTO LEVEL
will automatically trim the pitch angle when ANGLE or HORIZON flight modes are usedIf your old AKK VTX is not working, use vtx_smartaudio_early_akk_workaround
to fix it!
This adds the option to remove the first 2, 4, or 6 digits from the OSD plus code. Doing so requires a reference location (for example your current location when using Google Maps on your phone) within ~800, ~40, and ~2km, respectively.
Throttle smoothing in the navigation modes on fixed-wing aircraft is now enabled by default. This results in smoother throttle management and more efficient cruising.
In ACRO mode, you can mitigate the problem of the rudder fighting bank-and-yank turns by disabling the I-term when the bank angle is above a given threshold. Set the desired bank angle threshold on the Mechanics tab under PID tuning. 10 degrees is a good starting point. In the navigation modes, rudder handling is improved. As a consequence of this improvement, TURN ASSIST can no longer be used in ACRO mode.
INAV 3.0 supports, as an experimental feature, external BNO055 connected as either I2C or Serial device. Data from BNO055 can be used to display Artificial Horizon in OSD, Heading in OSD or drive the self-leveling ANGLE and HORIZON modes. Secondary IMU will not be used for navigation yet!
Via #4442 it is now possible to limit maximum altitude for both Fixed Wings and Multirotors. nav_max_altitude
sets the max altitude in centimeters. Bear in mind, limit is active only with Altitude Hold mode and does not affect manual and acro flight modes
INAV 3.0 comes with 4 general-purpose, user-programmable PID controllers that can be integrated with Logic Conditions and Global Variables. Why? Because why not! With the ability to override RC channels with Logic Conditions you can program your own heading, speed, altitude, whatever control.
Cmake usage.md
for src/main/CMakeLists.txt
.
You can get more suggestions following this link too.
Published by DzikuVx over 3 years ago
Hello and welcome to INAV 3.0.0 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are no longer supported in INAV. If you are still using F3 boards, please migrate to F4 or F7.
The supporting code will be retained for a few more releases, but will not be maintained and is not guaranteed to build or work properly in the future.
There are now separate adjustments for D and CD/FF gains. This breaks compatibility with diff
s from previous releases. Check the adjustments tab in the configurator after restoring a diff
to makes sure they are set up correctly.
The OSD fonts have been improved (@Jettrel) and there are several new symbols. A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
We suggest NOT to do a full diff
or dump
upgrade. To get the best performance set up your aircraft from scratch. You can copy osd
, aux
, serial
, and mixer settings, as well as accelerometer and magnetometer calibration values from INAV 2.6, but other settings should be tuned again.
Please follow the instructions on this page.
Setting | Description |
---|---|
imu2 | Display the current status of the Secondary IMU |
imu2 fetch | Get calibration data from the Secondary IMU |
pid | Configure general purpose PID controllers. Refer to docs |
Setting | Description |
---|---|
blackbox_device | Default: target |
log_level | Default: ERROR |
nav_overrides_motor_stop | When set to OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect on NAV modes which take control of the throttle when combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV |
nav_rth_climb_first | New: ON_FW_SPIRAL
|
platform_type | Default: MULTIROTOR |
receiver_type | Default: target |
rssi_source | Default: AUTO |
Setting | Description |
---|---|
dji_speed_source | Sets the speed type displayed by the DJI OSD: GROUND, 3D, AIR Default: GROUND |
dshot_beeper_enabled | Whether using DShot motors as beepers is enabled Default: TRUE |
dshot_beeper_tone | Sets the DShot beeper tone Values: 1 - 5 Default: 1 |
fw_d_pitch | Fixed wing rate stabilisation D-gain for PITCH Default: 0 |
fw_d_roll | Fixed wing rate stabilisation D-gain for ROLL Default: 0 |
fw_d_yaw | Fixed wing rate stabilisation D-gain for YAW Default: 0 |
fw_level_pitch_trim | Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level Values: -10 - 10 Default: 0 |
fw_yaw_iterm_freeze_bank_angle | Yaw Iterm is frozen when bank angle is above this threshold [degrees]. This solves the problem of the rudder counteracting turns by partially disabling yaw stabilization when making banked turns. Setting to 0 (the default) disables this feature. Only applies when autopilot is not active and TURN ASSIST is disabled. Values: 0 - 90 Default: 0 |
gyro_abg_alpha | Alpha factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 1 Default: 0 |
gyro_abg_boost | Boost factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 2 Default: 0.35 |
gyro_abg_half_life | Sample half-life for Gyro Alpha-Beta-Gamma filter Values: 0 - 10 Default: 0.5 |
gyro_anti_aliasing_lpf_hz | Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz Values: 0 - 255 Default: 250 |
gyro_anti_aliasing_lpf_type | Specifies the type of the software LPF of the gyro signals. Default: PT1 |
gyro_dyn_lpf_curve_expo | Expo value for the throttle-to-frequency mapping for Dynamic LPF Values: 1 - 10 Default: 5 |
gyro_dyn_lpf_max_hz | Maximum frequency of the gyro Dynamic LPF Values: 40 - 1000 Default: 500 |
gyro_dyn_lpf_min_hz | Minimum frequency of the gyro Dynamic LPF Values: 40 - 400 Default: 200 |
gyro_main_lpf_hz | Software based gyro main lowpass filter. Value is cutoff frequency (Hz) Values: 0 - 500 Default: 60 |
gyro_main_lpf_type | Defines the type of the main gyro LPF filter. Possible values: PT1 , BIQUAD . PT1 offers faster filter response while BIQUAD better attenuation. Default: BIQUAD |
gyro_use_dyn_lpf | Use Dynamic LPF instead of static gyro stage1 LPF. Dynamic Gyro LPF updates gyro LPF based on the throttle position. Default: FALSE |
imu2_align_pitch | Pitch alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_roll | Roll alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_yaw | Yaw alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_gain_acc_x | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_y | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_z | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_x | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_y | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_z | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_hardware | Selection of a Secondary IMU hardware type. NONE disables this functionality Default: NONE, values NONE , BNO055 , BNO055_SERIAL
|
imu2_radius_acc | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_radius_mag | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_use_for_osd_ahi | If set to ON, Secondary IMU data will be used for Analog OSD Artificial Horizon Default: FALSE |
imu2_use_for_osd_heading | If set to ON, Secondary IMU data will be used for Analog OSD heading Default: FALSE |
imu2_use_for_stabilized | If set to ON, Secondary IMU data will be used for Angle, Horizon and all other modes that control attitude (PosHold, WP, RTH) Default: FALSE |
mavlink_version | Version of MAVLink to use Values: 1 - 2 Default: 2 |
nav_land_maxalt_vspd | Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s] Values: 100 - 2000 Default: 200 |
nav_land_minalt_vspd | Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s] Values: 50 - 500 Default: 50 |
nav_max_altitude | Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled Values: 0 - 65000 Default: 0 |
nav_mc_wp_slowdown | When ON, NAV engine will slow down when switching to the next waypoint. This prioritizes turning over forward movement. When OFF, NAV engine will continue to the next waypoint and turn as it goes. Default: TRUE |
nav_rth_alt_control_override | If set to ON RTH altitude and CLIMB FIRST settings can be overridden during the RTH climb phase using full pitch or roll stick held for > 1 second. RTH altitude is reset to the current altitude using pitch down stick. RTH CLIMB FIRST is overridden using right roll stick so craft turns and heads directly to home (CLIMB FIRST override only works for fixed wing) Default: FALSE |
osd_pan_servo_index | Index of the pan servo to adjust osd home heading direction based on camera pan. Note that this feature does not work with continiously rotating servos. Values: 0 - 10 Default: 0 |
osd_pan_servo_pwm2centideg | Centidegrees of pan servo rotation us PWM signal. A servo with 180 degrees of rotation from 1000 to 2000 us PWM typically needs 18 for this setting. Change sign to inverse direction. Values: -36 - 36 Default: 0 |
osd_plus_code_short | Number of leading digits removed from plus code. Removing 2, 4 and 6 digits requires a reference location within, respectively, ~800km, ~40 km and ~2km to recover the original coordinates. Default: 0 |
osd_sidebar_height | Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD) Values: 0 - 5 Default: 3 |
osd_stats_min_voltage_unit | Display minimum voltage of the BATTERY or the average per CELL in the OSD stats. Default: BATTERY. Options BATTERY , CELL
|
osd_telemetry | To enable OSD telemetry for antenna tracker. Possible values are OFF , ON and TEST Default: OFF |
prearm_timeout | Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout. Values: 0 - 10000 Default: 10000 |
safehome_max_distance | In order for a safehome to be used, it must be less than this distance (in cm) from the arming point. Values: 0 - 65000 Default: 20000 |
safehome_usage_mode | Used to control when safehomes will be used. Possible values are OFF , RTH and RTH_FS . See Safehome documentation for more information. Default: RTH |
servo_autotrim_rotation_limit | Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using feature FW_AUTOTRIM . Values: 1 - 60 Default: 15 |
smith_predictor_delay | Expected delay of the gyro signal. In milliseconds Values: 0 - 8 Default: 0 |
smith_predictor_lpf_hz | Cutoff frequency for the Smith Predictor Low Pass Filter Values: 1 - 500 Default: 50 |
smith_predictor_strength | The strength factor of a Smith Predictor of PID measurement. In percents Values: 0 - 1 Default: 0.5 |
turtle_mode_power_factor | Turtle mode power factor Values: 0 - 100 Default: 55 |
vtx_smartaudio_early_akk_workaround | Enable workaround for early AKK SAudio-enabled VTX bug. Default: TRUE |
osd_rssi_dbm_alarm | RSSI in dBm alarm for Crossfire. Default: 0 |
nav_wp_load_on_boot | If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup. Default: OFF |
Setting | Description |
---|---|
gyro_sync | |
nav_landing_speed | replaced by nav_land_minalt_vspd and nav_land_maxalt_vspd
|
Old name | New name |
---|---|
gyro_lpf_hz | Replaced with gyro_main_lpf_hz
|
gyro_lpf_type | Replaced with gyro_main_lpf_type
|
gyro_stage2_lowpass_hz | Replaced with gyro_anti_aliasing_lpf_hz
|
gyro_stage2_lowpass_type | Replaced with gyro_anti_aliasing_lpf_type
|
mc_airmode_threshold | airmode_threshold |
mc_airmode_type | airmode_type |
osd_artificial_horizon_max_pitch | osd_ahi_max_pitch |
osd_artificial_horizon_reverse_roll | osd_ahi_reverse_roll |
INAV now has a "Turtle Mode".
Prior to inav 3.0, mission waypoint altitudes are relative the arming location. It is now possible to define waypoints with absolute (AMSL) altitude, making the mission independent of the arming location. See the inav wiki for details (WP paramater 3
)
The relative / absolute ground altitude of a LAND
waypoint may be set as WP paramater 2
(m). See the inav wiki for details.
Nothing to add. If DSHOT is enabled, DSHOT beeper will be used.
MAVLink is still only a downlink from UAV to the ground station, but now allows to use RC-Over-MAVLink
Prearm offers a two-stage arming process as an optional additional safety feature.
H7 is available in the source repository; target Hex files will be released as targets mature, probably in the future point releases.
You can now use the D-gain to improve the stabilization, especially on small and agile airplanes. Until we have a better understanding of how to tune this on a range of airplanes, the D-gain is set to zero by default and not tuned using autotune. Please report good performing tunes in https://github.com/iNavFlight/inav/issues/6709.
AUTOTUNE can now automatically set the correct rates for your airplane. The goal is to set rates that the airplane is capable of achieving with 80% control surface deflection so there is some room for the stabilization to work. This feature is controlled by CLI setting fw_autotune_rate_adjustment
. When set to AUTO
(the default), autotune automatically determines the rates and gains. When set to MAX
, rates will be automatically adjusted, but never above the starting values. This can be used to calm down a very agile plane, while still avoiding setting too high rates. When set to FIXED
, rates will not be adjusted. Note that setting too high rates can cause very bad flight behavior and potential crashes. Rate discovery is not possible in ANGLE mode so it is highly advised to do autotune in ACRO mode.
There is now the option to continuously trim the servos for straight and level flight. When enabled and flying straight and level, INAV records what servo output is required to maintain a constant attitude, and adjusts the servo midpoints accordingly. The servo midpoints are limited to the 1300-1700 range. After the first maiden flight, and after the first flight when significant changes have been made to the airplane, check the servo midpoints. If they are at or close to the end of this range mechanically adjust the control surfaces.
As part of gyro processing updates, the following changes were made:
gyro_sync
is gone, INAV no longer does a wait cycle trying to get the next set of data from the gyro.gyro_anti_aliasing_lpf_hz
). In normal circumstances, there is no need to change this settinggyro_lpf_hz
was renamed to gyro_main_lpf_hz
set smith_predictor_delay = 3
. More details about this feature will follow laterset gyro_abg_alpha = 0.25
or higher value. It requires a very clean gyro signal or might introduce oscillations on the high throttle. If the multirotor started to vibrate after enabling the Alpha-Beta-Gamma filter, you either have to improve the gyro filter strategy or disable the ABG filter. It works great on some builds and not so great or other. It's up to you to test.set gyro_use_dyn_lpf=ON
and set gyro_dyn_lpf_min_hz
and gyro_dyn_lpf_max_hz
. Dynamic LPF replaces gyro_main_lpf_hz
The EGNOS (GPS ground assistance) definitions have been updated to the latest values for all GNSS options. An invalid association with the availability of Galileo has been corrected.
New FCs rarely feature onboard compass, and most GPS+MAG default to CW270FLIP, so this is now the INAV default. If you use another value, check your setup after upgrading.
To more clearly state what they do and how they work. It's a subtle, but worth it to change for sure!
Users must upgrade OSD Fonts to Version 2 (or later).
Safehome does not now replace the arming location until it is needed. If you cancel RTH or recover from RX failsafe, the original arming location is restored as the home location. Under normal circumstances, "distance to home" will revert to range from the arming location.
Provides stick options to override configured RTH climb and/or turn behaviour. See the nav_rth_alt_control_override
setting description for details.
Modes names were changed to be more user friendly. When OSD OFF
is enabled, OSD will be turned off. When LED OFF
is enabled, LEDs will be turned off.
Yeap, now when nav_rth_climb_first
is set to ON_FW_SPIRAL
, Fixed Wing will keep litering and gaining altitude until it reaches desired altitude. Previously, it was climbing while flying straight in random direction
When nav_mc_wp_slowdown
is set to OFF
, Waypoint missions on Multirotors will be smoother as the NAV engine will not try to slow down before entering the waypoint and then accelerate towards the next waypoint. INAV will rather enter WP with normal speed, switch to the next waypoint and then adjust heading while flying.
The default behavior of the DJI OSD speed element was to display a ground speed. osd_speed_source
can be set to GROUND, AIR or 3D speed depending on the preference
fw_level_pitch_trim
setting. +5 fw_level_pitch_trim
means airplane nose should be raised 5 deg from levelAUTO LEVEL
will automatically trim the pitch angle when ANGLE or HORIZON flight modes are usedIf your old AKK VTX is not working, use vtx_smartaudio_early_akk_workaround
to fix it!
This adds the option to remove the first 2, 4, or 6 digits from the OSD plus code. Doing so requires a reference location (for example your current location when using Google Maps on your phone) within ~800, ~40, and ~2km, respectively.
Throttle smoothing in the navigation modes on fixed wing aircraft is now enabled by default. This results in smoother throttle management and more efficient cruising.
In ACRO mode, you can mitigate the problem of the rudder fighting bank-and-yank turns by disabling the I-term when the bank angle is above a given threshold. Set the desired bank angle threshold on the Mechanics tab under PID tuning. 10 degrees is a good starting point. In the navigation modes, rudder handling is improved. As a consequence of this improvement, TURN ASSIST can no longer be used in ACRO mode.
INAV 3.0 supports, as an experimental feature, external BNO055 connected as either I2C or Serial device. Data from BNO055 can be used to display Artificial Horizon in OSD, Heading in OSD or drive the self-leveling ANGLE and HORIZON modes. Secondary IMU will not be used for navigation yet!
Via #4442 it is now possible to limit maximum altitude for both Fixed Wings and Multirotors. nav_max_altitude
sets the max altitude in centimeters. Bear in mind, limit is active only with Altitude Hold mode and does not affect manual and acro flight modes
INAV 3.0 comes with 4 general-purpose, user-programmable PID controllers that can be integrated with Logic Conditions and Global Variables. Why? Because why not! With the ability to override RC channels with Logic Conditions you can program your own heading, speed, altitude, whatever control.
Cmake usage.md
for src/main/CMakeLists.txt
.
You can get more suggestions following this link too.
Published by DzikuVx over 3 years ago
Hello and welcome to INAV 3.0.0 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are no longer supported in INAV. If you are still using F3 boards, please migrate to F4 or F7.
The supporting code will be retained for a few more releases, but will not be maintained and is not guaranteed to build or work properly in the future.
There are now separate adjustments for D and CD/FF gains. This breaks compatibility with diff
s from previous releases. Check the adjustments tab in the configurator after restoring a diff
to makes sure they are set up correctly.
The OSD fonts have been improved (@Jettrel) and there are several new symbols. A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
We suggest NOT to do a full diff
or dump
upgrade. To get the best performance set up your aircraft from scratch. You can copy osd
, aux
, serial
, and mixer settings, as well as accelerometer and magnetometer calibration values from INAV 2.6, but other settings should be tuned again.
Please follow the instructions on this page.
Setting | Description |
---|---|
imu2 | Display the current status of the Secondary IMU |
imu2 fetch | Get calibration data from the Secondary IMU |
pid | Configure general purpose PID controllers. Refer to docs |
Setting | Description |
---|---|
blackbox_device | Default: target |
log_level | Default: ERROR |
nav_overrides_motor_stop | When set to OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect on NAV modes which take control of the throttle when combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV |
nav_rth_climb_first | New: ON_FW_SPIRAL
|
platform_type | Default: MULTIROTOR |
receiver_type | Default: target |
rssi_source | Default: AUTO |
Setting | Description |
---|---|
dji_speed_source | Sets the speed type displayed by the DJI OSD: GROUND, 3D, AIR Default: GROUND |
dshot_beeper_enabled | Whether using DShot motors as beepers is enabled Default: TRUE |
dshot_beeper_tone | Sets the DShot beeper tone Values: 1 - 5 Default: 1 |
fw_d_pitch | Fixed wing rate stabilisation D-gain for PITCH Default: 0 |
fw_d_roll | Fixed wing rate stabilisation D-gain for ROLL Default: 0 |
fw_d_yaw | Fixed wing rate stabilisation D-gain for YAW Default: 0 |
fw_level_pitch_trim | Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level Values: -10 - 10 Default: 0 |
fw_yaw_iterm_freeze_bank_angle | Yaw Iterm is frozen when bank angle is above this threshold [degrees]. This solves the problem of the rudder counteracting turns by partially disabling yaw stabilization when making banked turns. Setting to 0 (the default) disables this feature. Only applies when autopilot is not active and TURN ASSIST is disabled. Values: 0 - 90 Default: 0 |
gyro_abg_alpha | Alpha factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 1 Default: 0 |
gyro_abg_boost | Boost factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 2 Default: 0.35 |
gyro_abg_half_life | Sample half-life for Gyro Alpha-Beta-Gamma filter Values: 0 - 10 Default: 0.5 |
gyro_anti_aliasing_lpf_hz | Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz Values: 0 - 255 Default: 250 |
gyro_anti_aliasing_lpf_type | Specifies the type of the software LPF of the gyro signals. Default: PT1 |
gyro_dyn_lpf_curve_expo | Expo value for the throttle-to-frequency mapping for Dynamic LPF Values: 1 - 10 Default: 5 |
gyro_dyn_lpf_max_hz | Maximum frequency of the gyro Dynamic LPF Values: 40 - 1000 Default: 500 |
gyro_dyn_lpf_min_hz | Minimum frequency of the gyro Dynamic LPF Values: 40 - 400 Default: 200 |
gyro_main_lpf_hz | Software based gyro main lowpass filter. Value is cutoff frequency (Hz) Values: 0 - 500 Default: 60 |
gyro_main_lpf_type | Defines the type of the main gyro LPF filter. Possible values: PT1 , BIQUAD . PT1 offers faster filter response while BIQUAD better attenuation. Default: BIQUAD |
gyro_use_dyn_lpf | Use Dynamic LPF instead of static gyro stage1 LPF. Dynamic Gyro LPF updates gyro LPF based on the throttle position. Default: FALSE |
imu2_align_pitch | Pitch alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_roll | Roll alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_yaw | Yaw alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_gain_acc_x | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_y | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_z | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_x | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_y | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_z | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_hardware | Selection of a Secondary IMU hardware type. NONE disables this functionality Default: NONE, values NONE , BNO055 , BNO055_SERIAL
|
imu2_radius_acc | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_radius_mag | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_use_for_osd_ahi | If set to ON, Secondary IMU data will be used for Analog OSD Artificial Horizon Default: FALSE |
imu2_use_for_osd_heading | If set to ON, Secondary IMU data will be used for Analog OSD heading Default: FALSE |
imu2_use_for_stabilized | If set to ON, Secondary IMU data will be used for Angle, Horizon and all other modes that control attitude (PosHold, WP, RTH) Default: FALSE |
mavlink_version | Version of MAVLink to use Values: 1 - 2 Default: 2 |
nav_land_maxalt_vspd | Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s] Values: 100 - 2000 Default: 200 |
nav_land_minalt_vspd | Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s] Values: 50 - 500 Default: 50 |
nav_max_altitude | Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled Values: 0 - 65000 Default: 0 |
nav_mc_wp_slowdown | When ON, NAV engine will slow down when switching to the next waypoint. This prioritizes turning over forward movement. When OFF, NAV engine will continue to the next waypoint and turn as it goes. Default: TRUE |
nav_rth_alt_control_override | If set to ON RTH altitude and CLIMB FIRST settings can be overridden during the RTH climb phase using full pitch or roll stick held for > 1 second. RTH altitude is reset to the current altitude using pitch down stick. RTH CLIMB FIRST is overridden using right roll stick so craft turns and heads directly to home (CLIMB FIRST override only works for fixed wing) Default: FALSE |
osd_pan_servo_index | Index of the pan servo to adjust osd home heading direction based on camera pan. Note that this feature does not work with continiously rotating servos. Values: 0 - 10 Default: 0 |
osd_pan_servo_pwm2centideg | Centidegrees of pan servo rotation us PWM signal. A servo with 180 degrees of rotation from 1000 to 2000 us PWM typically needs 18 for this setting. Change sign to inverse direction. Values: -36 - 36 Default: 0 |
osd_plus_code_short | Number of leading digits removed from plus code. Removing 2, 4 and 6 digits requires a reference location within, respectively, ~800km, ~40 km and ~2km to recover the original coordinates. Default: 0 |
osd_sidebar_height | Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD) Values: 0 - 5 Default: 3 |
osd_stats_min_voltage_unit | Display minimum voltage of the BATTERY or the average per CELL in the OSD stats. Default: BATTERY. Options BATTERY , CELL
|
osd_telemetry | To enable OSD telemetry for antenna tracker. Possible values are OFF , ON and TEST Default: OFF |
prearm_timeout | Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout. Values: 0 - 10000 Default: 10000 |
safehome_max_distance | In order for a safehome to be used, it must be less than this distance (in cm) from the arming point. Values: 0 - 65000 Default: 20000 |
safehome_usage_mode | Used to control when safehomes will be used. Possible values are OFF , RTH and RTH_FS . See Safehome documentation for more information. Default: RTH |
servo_autotrim_rotation_limit | Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using feature FW_AUTOTRIM . Values: 1 - 60 Default: 15 |
smith_predictor_delay | Expected delay of the gyro signal. In milliseconds Values: 0 - 8 Default: 0 |
smith_predictor_lpf_hz | Cutoff frequency for the Smith Predictor Low Pass Filter Values: 1 - 500 Default: 50 |
smith_predictor_strength | The strength factor of a Smith Predictor of PID measurement. In percents Values: 0 - 1 Default: 0.5 |
turtle_mode_power_factor | Turtle mode power factor Values: 0 - 100 Default: 55 |
vtx_smartaudio_early_akk_workaround | Enable workaround for early AKK SAudio-enabled VTX bug. Default: TRUE |
osd_rssi_dbm_alarm | RSSI in dBm alarm for Crossfire. Default: 0 |
nav_wp_load_on_boot | If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup. Default: OFF |
Setting | Description |
---|---|
gyro_sync | |
nav_landing_speed | replaced by nav_land_minalt_vspd and nav_land_maxalt_vspd
|
Old name | New name |
---|---|
gyro_lpf_hz | Replaced with gyro_main_lpf_hz
|
gyro_lpf_type | Replaced with gyro_main_lpf_type
|
gyro_stage2_lowpass_hz | Replaced with gyro_anti_aliasing_lpf_hz
|
gyro_stage2_lowpass_type | Replaced with gyro_anti_aliasing_lpf_type
|
mc_airmode_threshold | airmode_threshold |
mc_airmode_type | airmode_type |
osd_artificial_horizon_max_pitch | osd_ahi_max_pitch |
osd_artificial_horizon_reverse_roll | osd_ahi_reverse_roll |
INAV now has a "Turtle Mode".
Prior to inav 3.0, mission waypoint altitudes are relative the arming location. It is now possible to define waypoints with absolute (AMSL) altitude, making the mission independent of the arming location. See the inav wiki for details (WP paramater 3
)
The relative / absolute ground altitude of a LAND
waypoint may be set as WP paramater 2
(m). See the inav wiki for details.
Nothing to add. If DSHOT is enabled, DSHOT beeper will be used.
MAVLink is still only a downlink from UAV to the ground station, but now allows to use RC-Over-MAVLink
Prearm offers a two-stage arming process as an optional additional safety feature.
H7 is available in the source repository; target Hex files will be released as targets mature, probably in the future point releases.
You can now use the D-gain to improve the stabilization, especially on small and agile airplanes. Until we have a better understanding of how to tune this on a range of airplanes, the D-gain is set to zero by default and not tuned using autotune. Please report good performing tunes in https://github.com/iNavFlight/inav/issues/6709.
AUTOTUNE can now automatically set the correct rates for your airplane. The goal is to set rates that the airplane is capable of achieving with 80% control surface deflection so there is some room for the stabilization to work. This feature is controlled by CLI setting fw_autotune_rate_adjustment
. When set to AUTO
(the default), autotune automatically determines the rates and gains. When set to MAX
, rates will be automatically adjusted, but never above the starting values. This can be used to calm down a very agile plane, while still avoiding setting too high rates. When set to FIXED
, rates will not be adjusted. Note that setting too high rates can cause very bad flight behavior and potential crashes. Rate discovery is not possible in ANGLE mode so it is highly advised to do autotune in ACRO mode.
There is now the option to continuously trim the servos for straight and level flight. When enabled and flying straight and level, INAV records what servo output is required to maintain a constant attitude, and adjusts the servo midpoints accordingly. The servo midpoints are limited to the 1300-1700 range. After the first maiden flight, and after the first flight when significant changes have been made to the airplane, check the servo midpoints. If they are at or close to the end of this range mechanically adjust the control surfaces.
As part of gyro processing updates, the following changes were made:
gyro_sync
is gone, INAV no longer does a wait cycle trying to get the next set of data from the gyro.gyro_anti_aliasing_lpf_hz
). In normal circumstances, there is no need to change this settinggyro_lpf_hz
was renamed to gyro_main_lpf_hz
set smith_predictor_delay = 3
. More details about this feature will follow laterset gyro_abg_alpha = 0.25
or higher value. It requires a very clean gyro signal or might introduce oscillations on the high throttle. If the multirotor started to vibrate after enabling the Alpha-Beta-Gamma filter, you either have to improve the gyro filter strategy or disable the ABG filter. It works great on some builds and not so great or other. It's up to you to test.set gyro_use_dyn_lpf=ON
and set gyro_dyn_lpf_min_hz
and gyro_dyn_lpf_max_hz
. Dynamic LPF replaces gyro_main_lpf_hz
The EGNOS (GPS ground assistance) definitions have been updated to the latest values for all GNSS options. An invalid association with the availability of Galileo has been corrected.
New FCs rarely feature onboard compass, and most GPS+MAG default to CW270FLIP, so this is now the INAV default. If you use another value, check your setup after upgrading.
To more clearly state what they do and how they work. It's a subtle, but worth it to change for sure!
Users must upgrade OSD Fonts to Version 2 (or later).
Safehome does not now replace the arming location until it is needed. If you cancel RTH or recover from RX failsafe, the original arming location is restored as the home location. Under normal circumstances, "distance to home" will revert to range from the arming location.
Provides stick options to override configured RTH climb and/or turn behaviour. See the nav_rth_alt_control_override
setting description for details.
Modes names were changed to be more user friendly. When OSD OFF
is enabled, OSD will be turned off. When LED OFF
is enabled, LEDs will be turned off.
Yeap, now when nav_rth_climb_first
is set to ON_FW_SPIRAL
, Fixed Wing will keep litering and gaining altitude until it reaches desired altitude. Previously, it was climbing while flying straight in random direction
When nav_mc_wp_slowdown
is set to OFF
, Waypoint missions on Multirotors will be smoother as the NAV engine will not try to slow down before entering the waypoint and then accelerate towards the next waypoint. INAV will rather enter WP with normal speed, switch to the next waypoint and then adjust heading while flying.
The default behavior of the DJI OSD speed element was to display a ground speed. osd_speed_source
can be set to GROUND, AIR or 3D speed depending on the preference
fw_level_pitch_trim
setting. +5 fw_level_pitch_trim
means airplane nose should be raised 5 deg from levelAUTO LEVEL
will automatically trim the pitch angle when ANGLE or HORIZON flight modes are usedIf your old AKK VTX is not working, use vtx_smartaudio_early_akk_workaround
to fix it!
This adds the option to remove the first 2, 4, or 6 digits from the OSD plus code. Doing so requires a reference location (for example your current location when using Google Maps on your phone) within ~800, ~40, and ~2km, respectively.
Throttle smoothing in the navigation modes on fixed wing aircraft is now enabled by default. This results in smoother throttle management and more efficient cruising.
In ACRO mode, you can mitigate the problem of the rudder fighting bank-and-yank turns by disabling the I-term when the bank angle is above a given threshold. Set the desired bank angle threshold on the Mechanics tab under PID tuning. 10 degrees is a good starting point. In the navigation modes, rudder handling is improved. As a consequence of this improvement, TURN ASSIST can no longer be used in ACRO mode.
INAV 3.0 supports, as an experimental feature, external BNO055 connected as either I2C or Serial device. Data from BNO055 can be used to display Artificial Horizon in OSD, Heading in OSD or drive the self-leveling ANGLE and HORIZON modes. Secondary IMU will not be used for navigation yet!
Via #4442 it is now possible to limit maximum altitude for both Fixed Wings and Multirotors. nav_max_altitude
sets the max altitude in centimeters. Bear in mind, limit is active only with Altitude Hold mode and does not affect manual and acro flight modes
INAV 3.0 comes with 4 general-purpose, user-programmable PID controllers that can be integrated with Logic Conditions and Global Variables. Why? Because why not! With the ability to override RC channels with Logic Conditions you can program your own heading, speed, altitude, whatever control.
Cmake usage.md
for src/main/CMakeLists.txt
.
You can get more suggestions following this link too.
Published by DzikuVx over 3 years ago
Hello and welcome to INAV 3.0.0 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are no longer supported in INAV. If you are still using F3 boards, please migrate to F4 or F7.
The supporting code will be retained for a few more releases, but will not be maintained and is not guaranteed to build or work properly in the future.
There are now separate adjustments for D and CD/FF gains. This breaks compatibility with diff
s from previous releases. Check the adjustments tab in the configurator after restoring a diff
to makes sure they are set up correctly.
The OSD fonts have been improved (@Jettrel) and there are several new symbols. A font file update is required to use the new symbols and avoid an invalid font warning. Upload the updated font of your choosing from the OSD tab.
We suggest NOT to do a full diff
or dump
upgrade. To get the best performance set up your aircraft from scratch. You can copy osd
, aux
, serial
, and mixer settings, as well as accelerometer and magnetometer calibration values from INAV 2.6, but other settings should be tuned again.
Please follow the instructions on this page.
Setting | Description |
---|---|
imu2 | Display current status of the Secondary IMU |
imu2 fetch | Get calibration data from the Secondary IMU |
pid | Configure general purpose PID controllers. Refer to docs |
Setting | Description |
---|---|
blackbox_device | Default: target |
log_level | Default: ERROR |
nav_overrides_motor_stop | When set to OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect on NAV modes which take control of the throttle when combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV |
nav_rth_climb_first | New: ON_FW_SPIRAL
|
platform_type | Default: MULTIROTOR |
receiver_type | Default: target |
rssi_source | Default: AUTO |
Setting | Description |
---|---|
dji_speed_source | Sets the speed type displayed by the DJI OSD: GROUND, 3D, AIR Default: GROUND |
dshot_beeper_enabled | Whether using DShot motors as beepers is enabled Default: TRUE |
dshot_beeper_tone | Sets the DShot beeper tone Values: 1 - 5 Default: 1 |
fw_d_pitch | Fixed wing rate stabilisation D-gain for PITCH Default: 0 |
fw_d_roll | Fixed wing rate stabilisation D-gain for ROLL Default: 0 |
fw_d_yaw | Fixed wing rate stabilisation D-gain for YAW Default: 0 |
fw_level_pitch_trim | Pitch trim for self-leveling flight modes. In degrees. +5 means airplane nose should be raised 5 deg from level Values: -10 - 10 Default: 0 |
fw_yaw_iterm_freeze_bank_angle | Yaw Iterm is frozen when bank angle is above this threshold [degrees]. This solves the problem of the rudder counteracting turns by partially disabling yaw stabilization when making banked turns. Setting to 0 (the default) disables this feature. Only applies when autopilot is not active and TURN ASSIST is disabled. Values: 0 - 90 Default: 0 |
gyro_abg_alpha | Alpha factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 1 Default: 0 |
gyro_abg_boost | Boost factor for Gyro Alpha-Beta-Gamma filter Values: 0 - 2 Default: 0.35 |
gyro_abg_half_life | Sample half-life for Gyro Alpha-Beta-Gamma filter Values: 0 - 10 Default: 0.5 |
gyro_anti_aliasing_lpf_hz | Gyro processing anti-aliasing filter cutoff frequency. In normal operation this filter setting should never be changed. In Hz Values: 0 - 255 Default: 250 |
gyro_anti_aliasing_lpf_type | Specifies the type of the software LPF of the gyro signals. Default: PT1 |
gyro_dyn_lpf_curve_expo | Expo value for the throttle-to-frequency mapping for Dynamic LPF Values: 1 - 10 Default: 5 |
gyro_dyn_lpf_max_hz | Maximum frequency of the gyro Dynamic LPF Values: 40 - 1000 Default: 500 |
gyro_dyn_lpf_min_hz | Minimum frequency of the gyro Dynamic LPF Values: 40 - 400 Default: 200 |
gyro_main_lpf_hz | Software based gyro main lowpass filter. Value is cutoff frequency (Hz) Values: 0 - 500 Default: 60 |
gyro_main_lpf_type | Defines the type of the main gyro LPF filter. Possible values: PT1 , BIQUAD . PT1 offers faster filter response while BIQUAD better attenuation. Default: BIQUAD |
gyro_use_dyn_lpf | Use Dynamic LPF instead of static gyro stage1 LPF. Dynamic Gyro LPF updates gyro LPF based on the throttle position. Default: FALSE |
imu2_align_pitch | Pitch alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_roll | Roll alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_align_yaw | Yaw alignment for Secondary IMU. 1/10 of a degree Values: -1800 - 3600 Default: 0 |
imu2_gain_acc_x | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_y | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_acc_z | Secondary IMU ACC calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_x | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_y | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_gain_mag_z | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_hardware | Selection of a Secondary IMU hardware type. NONE disables this functionality Default: NONE, values NONE , BNO055 , BNO055_SERIAL
|
imu2_radius_acc | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_radius_mag | Secondary IMU MAG calibration data Values: -32768 - 32767 Default: 0 |
imu2_use_for_osd_ahi | If set to ON, Secondary IMU data will be used for Analog OSD Artificial Horizon Default: FALSE |
imu2_use_for_osd_heading | If set to ON, Secondary IMU data will be used for Analog OSD heading Default: FALSE |
imu2_use_for_stabilized | If set to ON, Secondary IMU data will be used for Angle, Horizon and all other modes that control attitude (PosHold, WP, RTH) Default: FALSE |
mavlink_version | Version of MAVLink to use Values: 1 - 2 Default: 2 |
nav_land_maxalt_vspd | Vertical descent velocity above nav_land_slowdown_maxalt during the RTH landing phase. [cm/s] Values: 100 - 2000 Default: 200 |
nav_land_minalt_vspd | Vertical descent velocity under nav_land_slowdown_minalt during the RTH landing phase. [cm/s] Values: 50 - 500 Default: 50 |
nav_max_altitude | Max allowed altitude (above Home Point) that applies to all NAV modes (including Altitude Hold). 0 means limit is disabled Values: 0 - 65000 Default: 0 |
nav_mc_wp_slowdown | When ON, NAV engine will slow down when switching to the next waypoint. This prioritizes turning over forward movement. When OFF, NAV engine will continue to the next waypoint and turn as it goes. Default: TRUE |
nav_rth_alt_control_override | If set to ON RTH altitude and CLIMB FIRST settings can be overridden during the RTH climb phase using full pitch or roll stick held for > 1 second. RTH altitude is reset to the current altitude using pitch down stick. RTH CLIMB FIRST is overridden using right roll stick so craft turns and heads directly to home (CLIMB FIRST override only works for fixed wing) Default: FALSE |
osd_pan_servo_index | Index of the pan servo to adjust osd home heading direction based on camera pan. Note that this feature does not work with continiously rotating servos. Values: 0 - 10 Default: 0 |
osd_pan_servo_pwm2centideg | Centidegrees of pan servo rotation us PWM signal. A servo with 180 degrees of rotation from 1000 to 2000 us PWM typically needs 18 for this setting. Change sign to inverse direction. Values: -36 - 36 Default: 0 |
osd_plus_code_short | Number of leading digits removed from plus code. Removing 2, 4 and 6 digits requires a reference location within, respectively, ~800km, ~40 km and ~2km to recover the original coordinates. Default: 0 |
osd_sidebar_height | Height of sidebars in rows. 0 leaves only the level indicator arrows (Not for pixel OSD) Values: 0 - 5 Default: 3 |
osd_stats_min_voltage_unit | Display minimum voltage of the BATTERY or the average per CELL in the OSD stats. Default: BATTERY. Options BATTERY , CELL
|
osd_telemetry | To enable OSD telemetry for antenna tracker. Possible values are OFF , ON and TEST Default: OFF |
prearm_timeout | Duration (ms) for which Prearm being activated is valid. after this, Prearm needs to be reset. 0 means Prearm does not timeout. Values: 0 - 10000 Default: 10000 |
safehome_max_distance | In order for a safehome to be used, it must be less than this distance (in cm) from the arming point. Values: 0 - 65000 Default: 20000 |
safehome_usage_mode | Used to control when safehomes will be used. Possible values are OFF , RTH and RTH_FS . See Safehome documentation for more information. Default: RTH |
servo_autotrim_rotation_limit | Servo midpoints are only updated when total aircraft rotation is less than this threshold [deg/s]. Only applies when using feature FW_AUTOTRIM . Values: 1 - 60 Default: 15 |
smith_predictor_delay | Expected delay of the gyro signal. In milliseconds Values: 0 - 8 Default: 0 |
smith_predictor_lpf_hz | Cutoff frequency for the Smith Predictor Low Pass Filter Values: 1 - 500 Default: 50 |
smith_predictor_strength | The strength factor of a Smith Predictor of PID measurement. In percents Values: 0 - 1 Default: 0.5 |
turtle_mode_power_factor | Turtle mode power factor Values: 0 - 100 Default: 55 |
vtx_smartaudio_early_akk_workaround | Enable workaround for early AKK SAudio-enabled VTX bug. Default: TRUE |
osd_rssi_dbm_alarm | RSSI in dBm alarm for Crossfire. Default: 0 |
nav_wp_load_on_boot | If set to ON, waypoints will be automatically loaded from EEPROM to the FC during startup. Default: OFF |
Setting | Description |
---|---|
gyro_sync | |
nav_landing_speed | replaced by nav_land_minalt_vspd and nav_land_maxalt_vspd
|
Old name | New name |
---|---|
gyro_lpf_hz | Replaced with gyro_main_lpf_hz
|
gyro_lpf_type | Replaced with gyro_main_lpf_type
|
gyro_stage2_lowpass_hz | Replaced with gyro_anti_aliasing_lpf_hz
|
gyro_stage2_lowpass_type | Replaced with gyro_anti_aliasing_lpf_type
|
mc_airmode_threshold | airmode_threshold |
mc_airmode_type | airmode_type |
osd_artificial_horizon_max_pitch | osd_ahi_max_pitch |
osd_artificial_horizon_reverse_roll | osd_ahi_reverse_roll |
INAV now has a "Turtle Mode".
Prior to inav 3.0, mission waypoint altitudes are relative the arming location. It is now possible to define waypoints with absolute (AMSL) altitude, making the mission independent of the arming location. See the inav wiki for details (WP paramater 3
)
The relative / absolute ground altitude of a LAND
waypoint may be set as WP paramater 2
(m). See the inav wiki for details.
Nothing to add. If DSHOT is enabled, DSHOT beeper will be used.
MAVLink is still only a downlink from UAV to the ground station, but now allows to use RC-Over-MAVLink
Prearm offers a two-stage arming process as an optional additional safety feature.
H7 is available in the source repository; target Hex files will be released as targets mature, probably in the future point releases.
You can now use the D-gain to improve the stabilization, especially on small and agile airplanes. Until we have a better understanding of how to tune this on a range of airplanes, the D-gain is set to zero by default and not tuned using autotune. Please report good performing tunes in https://github.com/iNavFlight/inav/issues/6709.
AUTOTUNE can now automatically set the correct rates for your airplane. The goal is to set rates that the airplane is capable of achieving with 80% control surface deflection so there is some room for the stabilization to work. This feature is controlled by CLI setting fw_autotune_rate_adjustment
. When set to AUTO
(the default), autotune automatically determines the rates and gains. When set to MAX
, rates will be automatically adjusted, but never above the starting values. This can be used to calm down a very agile plane, while still avoiding setting too high rates. When set to FIXED
, rates will not be adjusted. Note that setting too high rates can cause very bad flight behavior and potential crashes. Rate discovery is not possible in ANGLE mode so it is highly advised to do autotune in ACRO mode.
There is now the option to continuously trim the servos for straight and level flight. When enabled and flying straight and level, INAV records what servo output is required to maintain a constant attitude, and adjusts the servo midpoints accordingly. The servo midpoints are limited to the 1300-1700 range. After the first maiden flight, and after the first flight when significant changes have been made to the airplane, check the servo midpoints. If they are at or close to the end of this range mechanically adjust the control surfaces.
As part of gyro processing updates, the following changes were made:
gyro_sync
is gone, INAV no longer does a wait cycle trying to get the next set of data from the gyro.gyro_anti_aliasing_lpf_hz
). In normal circumstances, there is no need to change this settinggyro_lpf_hz
was renamed to gyro_main_lpf_hz
set smith_predictor_delay = 3
. More details about this feature will follow laterset gyro_abg_alpha = 0.25
or higher value. It requires a very clean gyro signal or might introduce oscillations on the high throttle. If the multirotor started to vibrate after enabling the Alpha-Beta-Gamma filter, you either have to improve the gyro filter strategy or disable the ABG filter. It works great on some builds and not so great or other. It's up to you to test.set gyro_use_dyn_lpf=ON
and set gyro_dyn_lpf_min_hz
and gyro_dyn_lpf_max_hz
. Dynamic LPF replaces gyro_main_lpf_hz
The EGNOS (GPS ground assistance) definitions have been updated to the latest values for all GNSS options. An invalid association with the availability of Galileo has been corrected.
New FCs rarely feature onboard compass, and most GPS+MAG default to CW270FLIP, so this is now the INAV default. If you use another value, check your setup after upgrading.
To more clearly state what they do and how they work. It's a subtle, but worth it to change for sure!
Users must upgrade OSD Fonts to Version 2 (or later).
Safehome does not now replace the arming location until it is needed. If you cancel RTH or recover from RX failsafe, the original arming location is restored as the home location. Under normal circumstances, "distance to home" will revert to range from the arming location.
Provides stick options to override configured RTH climb and/or turn behaviour. See the nav_rth_alt_control_override
setting description for details.
Modes names were changed to be more user friendly. When OSD OFF
is enabled, OSD will be turned off. When LED OFF
is enabled, LEDs will be turned off.
Yeap, now when nav_rth_climb_first
is set to ON_FW_SPIRAL
, Fixed Wing will keep litering and gaining altitude until it reaches desired altitude. Previously, it was climbing while flying straight in random direction
When nav_mc_wp_slowdown
is set to OFF
, Waypoint missions on Multirotors will be smoother as the NAV engine will not try to slow down before entering the waypoint and then accelerate towards the next waypoint. INAV will rather enter WP with normal speed, switch to the next waypoint and then adjust heading while flying.
The default behavior of the DJI OSD speed element was to display a ground speed. osd_speed_source
can be set to GROUND, AIR or 3D speed depending on the preference
fw_level_pitch_trim
setting. +5 fw_level_pitch_trim
means airplane nose should be raised 5 deg from levelAUTO LEVEL
will automatically trim the pitch angle when ANGLE or HORIZON flight modes are usedIf your old AKK VTX is not working, use vtx_smartaudio_early_akk_workaround
to fix it!
This adds the option to remove the first 2, 4, or 6 digits from the OSD plus code. Doing so requires a reference location (for example your current location when using Google Maps on your phone) within ~800, ~40, and ~2km, respectively.
Throttle smoothing in the navigation modes on fixed wing aircraft is now enabled by default. This results in smoother throttle management and more efficient cruising.
In ACRO mode, you can mitigate the problem of the rudder fighting bank-and-yank turns by disabling the I-term when the bank angle is above a given threshold. Set the desired bank angle threshold on the Mechanics tab under PID tuning. 10 degrees is a good starting point. In the navigation modes, rudder handling is improved. As a consequence of this improvement, TURN ASSIST can no longer be used in ACRO mode.
INAV 3.0 supports, as an experimental feature, external BNO055 connected as either I2C or Serial device. Data from BNO055 can be used to display Artificial Horizon in OSD, Heading in OSD or drive the self-leveling ANGLE and HORIZON modes. Secondary IMU will not be used for navigation yet!
Via #4442 it is now possible to limit maximum altitude for both Fixed Wings and Multirotors. nav_max_altitude
sets the max altitude in centimeters. Bear in mind, limit is active only with Altitude Hold mode and does not affect manual and acro flight modes
INAV 3.0 comes with 4 general-purpose, user-programmable PID controllers that can be integrated with Logic Conditions and Global Variables. Why? Because why not! With the ability to override RC channels with Logic Conditions you can program your own heading, speed, altitude, whatever control.
Cmake usage.md
for src/main/CMakeLists.txt
.
You can get more suggestions following this link too.
Published by DzikuVx over 3 years ago
Hello and welcome to INAV 2.6.1 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
Compass has to be recalibrated. Do not import from previous INAV releases, even from 2.6.0
Do not migrate Multirotor PID and filter settings from previous releases of INAV. Use Multirotor default preset (3"-7") instead and make required changes on top of that
Setting | Description |
---|---|
serial_rx |
New option added GHST
|
baro_median_filter |
Default set back to ON
|
Setting | Description |
---|---|
osd_home_position_arm_screen |
Show GPS position on Arming Screen. Default ON
|
You can get more suggestions following this link too.
Published by digitalentity almost 4 years ago
Hello and welcome to INAV 2.6.0 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
Compass has to be recalibrated. Do not import from previous INAV releases
Do not migrate Multirotor PID and filter settings from previous releases of INAV. Use Multirotor default preset (3"-7") instead and make required changes on top of that
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are deprecated and soon they will reach the end of support in INAV. If you are still using F3 boards, please migrate to F4 or F7.
INAV 2.6 will be the last release that supports F3-based boards. The supporting code will be retained for a few more releases, but will not be maintained and is not guarantee to build or work properly in future releases.
In INAV 2.6, Logic Conditions and Global Functions have merged. Due to this the Global Functions from INAV 2.5 and below will not be added through the diff upgrade path.
If you previously used Global Functions, we would recommend taking a screen grab of your Global Functions in 2.5 before updating. Then in 2.6, add the Global Functions after the Logic Conditions on this programming page.
A new feature safehome
(see below) replaces nav_rth_home_offset_distance
and nav_rth_home_offset_direction
, offering a safer and much more flexible function. If you were using the nav_rth_home_offset_*
settings, please migrate to safehome
as these settings are removed.
Please follow the instructions on this page.
Command | Description |
---|---|
safehome |
List of home locations, see Safehomes.md and summary |
bind_rx |
Initiate binding for RX_SPI or SRXL2 receivers |
Setting | Description |
---|---|
mag_hardware |
New option added MSP
|
baro_hardware |
New options added DPS310 and MSP
|
pitot_hardware |
New options added MSP
|
serialrx_provider |
New options added FPORT2 and SRXL2
|
gps_provider |
New options added MSP
|
debug_mode |
New options added CD , KALMAN_GAIN , PID_MEASUREMENT , SPM_CELLS , SPM_VS600 , SPM_VARIO , PCF8574
|
airmode_type |
New option added STICK_CENTER_ONCE
|
nav_overrides_motor_stop |
Modified values OFF_ALWAYS , OFF , AUTO_ONLY , ALL_NAV . When set OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF always the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV. |
motor_pwm_protocol |
The default is now ONESHOT125 (previously STANDARD). |
Setting | Description |
---|---|
gyro_notch_hz |
Replaces gyro_notch1_hz and gyro_notch2_hz
|
gyro_notch_cutoff |
Replaces gyro_notch1_cutoff and gyro_notch2_cutoff
|
maggain_x , maggain_y , maggain_z
|
Calibrated values replacing fixed values. Compass re-calibration is required. |
srxl2_unit_id |
Values 0 - 15, default 1 |
srxl2_baud_fast |
Values OFF , ON , default ON
|
mc_cd_pitch |
Multicopter Control Derivative gain for PITCH, values 0 - 200, default 60 |
mc_cd_roll |
Multicopter Control Derivative gain for ROLL, values 0 - 200, default 60 |
mc_cd_yaw |
Multicopter Control Derivative gain for YAW, values 0 - 200, default 60 |
fw_turn_assist_pitch_gain |
Gain required to keep constant pitch angle during coordinated turns (in TURN_ASSIST mode). Value significantly different from 1.0 indicates a problem with the airspeed calibration (if present) or value of fw_reference_airspeed parameter. Values 0 - 2, default 1 |
nav_mc_vel_xy_dterm_attenuation |
Maximum D-term attenution percentage for horizontal velocity PID controller (Multirotor). It allows to smooth the PosHold CRUISE, WP and RTH when Multirotor is traveling at full speed. Dterm is not attenuated at low speeds, breaking and accelerating. Values 0 - 100, default 90 |
nav_mc_vel_xy_dterm_attenuation_start |
A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins. Values 0 - 100, default 10 |
nav_mc_vel_xy_dterm_attenuation_end |
A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm _attenuation reaches maximum. Values 0-100, default 60 |
mc_cd_lpf_hz |
Cutoff frequency for Control Derivative. Lower value smoother reaction on fast stick movements. With higher values, response will be more aggressive and jerky. Values 0 - 200, default 30 |
setpoint_kalman_enabled |
Enable Kalman filter on the PID controller setpoint. Values OFF , ON , default OFF
|
setpoint_kalman_q |
Quality factor of the setpoint Kalman filter. Higher values means less filtering and lower phase delay. On 3-7 inch multirotors can be usually increased to 200-300 or even higher on clean builds. Values 1 - 16000, default 100 |
setpoint_kalman_w |
Window size for the setpoint Kalman filter. Wider the window, more samples are used to compute variance. In general, wider window results in smoother filter response. Values 1 - 40, default 4 |
setpoint_kalman_sharpness |
Dynamic factor for the setpoint Kalman filter. In general, the higher the value, the more dynamic Kalman filter gets. Values 1 - 16000, default 100 |
inav_use_gps_no_baro |
Values OFF , ON , default OFF
|
nav_fw_pitch2thr_smoothing |
How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by nav_fw_pitch2thr_threshold . Values 0 - 9, default 0 |
nav_fw_pitch2thr_threshold |
Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees]. Values 0 - 900, default 0 |
nav_fw_launch_end_time |
Time for the transition of throttle and pitch angle, between the launch state and the subsequent flight mode [ms]. Values 0 - 5000, default 2000 |
mavlink_extra3_rate |
Values 0 - 255, default 1 |
osd_snr_alarm |
Value below which Crossfire SNR Alarm pops-up. (dB). Values -12 - 8, default 4 |
osd_link_quality_alarm |
LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%". Values 0 - 100, default 70 |
osd_crsf_lq_format |
OSD display format for CRSF LQ. Values TYPE1 or TYPE2
|
osd_force_grid |
Force OSD to work in grid mode even if the OSD device supports pixel level access (mainly used for development). Default OFF
|
osd_ahi_bordered |
Shows a border/corners around the AHI region (pixel OSD only). Default OFF
|
osd_ahi_width |
AHI width in pixels (pixel OSD only). Values 0 - 255, default 132 |
osd_ahi_height |
AHI width in pixels (pixel OSD only). Values 0 - 255, default 162 |
osd_ahi_vertical_offset |
AHI vertical offset from center (pixel OSD only). Values -128 - 127, default 0 |
osd_sidebar_horizontal_offset |
Sidebar horizontal offset from default position. Positive values move the sidebars closer to the edges. Values -128 - 127, default 0 |
osd_left_sidebar_scroll_step |
How many units each sidebar step represents. 0 means the default value for the scroll type. Values 0 - 255, default 0 |
osd_right_sidebar_scroll_step |
How many units each sidebar step represents. 0 means the default value for the scroll type. Values 0 - 255, default 0 |
smartport_master_halfduplex |
Values OFF , ON , default ON
|
smartport_master_inverted |
Values OFF , ON , default OFF
|
dji_esc_temp_source |
Re-purpose the ESC temperature field for IMU/BARO temperature. Values ESC , IMU , BARO , default ESC
|
dji_workarounds |
Enables workarounds for different versions of MSP protocol used. Values 0 - 255, default 1. May be set to 0 for non-DJI rigs, otherwise leave at default. |
dji_use_name_for_messages |
Re-purpose the craft name field for messages. Replace craft name with :WTSED for Warnings, Throttle, Speed, Efficiency, Trip distance. Values OFF , ON , default ON
|
Setting | Description |
---|---|
nav_rth_home_offset_distance |
Replaced by safehome
|
nav_rth_home_offset_direction |
Replaced by safehome
|
gyro_notch1_hz and gyro_notch2_hz
|
Replaced by gyro_notch_hz
|
gyro_notch1_cutoff and gyro_notch2_cutoff
|
Replaced by gyro_notch_cutoff
|
use_dterm_fir_filter |
|
dterm_setpoint_weight |
|
dterm_notch_hz |
|
dterm_notch_cutoff |
|
mc_iterm_relax_type |
The SET_POI
WP type defines a location for a point of interest (POI). The craft will fly the mission (until a SET_HEAD) with the nose pointing at the POI, which might be useful for aerial photography. Note that the craft does NOT fly to the POI. Wiki description and example.
The SET_HEAD
type sets the craft's heading (where it 'looks', not the direction of travel). This may be useful for useful for aerial photography. A value of -1
causing the heading to be 'straight ahead', i.e. the direction of travel. Thus, SET_POI
-1
may used to cancel a previous valid SET_HEAD
or SET_POI
. A SET_HEAD
remains in force until cancelled by SET_HEAD
with p1
of -1
, or modified by a subsequent SET_HEAD
or SET_POI
. Wiki description and example.
For now, this new waypoint types works only for multirotors, as this type of aircraft can fly "looking" to a different direction than it's flying. Different of an airplane, which can only fly forward and thus can only look forward when flying.
Safehome replaces the nav_rth_home_offset_*
settings, and allows the pilot to define up to 8 alternative home locations as absolute positions (lat, lon as decimal degress * 10,000,000). If a safehome
is within 200m of the arming point, it will be used as the home location for RTH etc. Please see the separate document Safehomes.md.
WP mode activation with no mission loaded previously kept the current flight mode which may be counter-intuitive to the pilot. OSD will show that the mode is kept, however WP missions are generally not FPV. This PR creates a fallback in such case and will execute RTH instead which is safer than let the drone drift away. Also fixes a bug when RTH procedure may get interrupted in case of a brief sensor loss and switch out to ANGLE, ACRO or MANUAL instead of EMERGENCY. On airplanes with a certain RTH settings a brief GPS loss is tolerated in the navigation state machine, while the RTH activation bug would still bail out. This PR fixes this by making RTH procedure sticky, similar to other navigation flight modes.
inav 2.6 updates the build environment to use cmake
as the build management tool. The developer build documentation has been updated for all platforms (MacOS, Linux, Windows, FreeBSD). Please see the platform specific documentation.
inav 2.6 can populate warnings and multiple (by DJI unsupported) OSD elements into the craft_name field.
Enable the feature via set dji_use_name_for_messages = ON
and configure the elements through the name
, considering:
set name = :WDSTE
You can get more suggestions following this link too.
Published by digitalentity almost 4 years ago
Hello and welcome to INAV 2.6.0 Release Candidate 3!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
Compass has to be recalibrated. Do not import from previous INAV releases
Do not migrate Multirotor PID and filter settings from previous releases of INAV. Use Multirotor default preset (3"-7") instead and make required changes on top of that
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are deprecated and soon they will reach the end of support in INAV. If you are still using F3 boards, please migrate to F4 or F7.
INAV 2.6 will be the last release that supports F3-based boards. The supporting code will be retained for a few more releases, but will not be maintained and is not guarantee to build or work properly in future releases.
A new feature safehome
(see below) replaces nav_rth_home_offset_distance
and nav_rth_home_offset_direction
, offering a safer and much more flexible function. If you were using the nav_rth_home_offset_*
settings, please migrate to safehome
as these settings are removed.
Please follow the instructions on this page.
Command | Description |
---|---|
safehome |
List of home locations, see Safehomes.md and summary |
bind_rx |
Initiate binding for RX_SPI or SRXL2 receivers |
Setting | Description |
---|---|
mag_hardware |
New option added MSP
|
baro_hardware |
New options added DPS310 and MSP
|
pitot_hardware |
New options added MSP
|
serialrx_provider |
New options added FPORT2 and SRXL2
|
gps_provider |
New options added MSP
|
debug_mode |
New options added CD , KALMAN_GAIN , PID_MEASUREMENT , SPM_CELLS , SPM_VS600 , SPM_VARIO , PCF8574
|
airmode_type |
New option added STICK_CENTER_ONCE
|
nav_overrides_motor_stop |
Modified values OFF , AUTO_ONLY , ALL_NAV . When set OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV. |
Setting | Description |
---|---|
gyro_notch_hz |
Replaces gyro_notch1_hz and gyro_notch2_hz
|
gyro_notch_cutoff |
Replaces gyro_notch1_cutoff and gyro_notch2_cutoff
|
maggain_x , maggain_y , maggain_z
|
Calibrated values replacing fixed values. Compass re-calibration is required. |
srxl2_unit_id |
Values 0 - 15, default 1 |
srxl2_baud_fast |
Values OFF , ON , default ON
|
mc_cd_pitch |
Multicopter Control Derivative gain for PITCH, values 0 - 200, default 60 |
mc_cd_roll |
Multicopter Control Derivative gain for ROLL, values 0 - 200, default 60 |
mc_cd_yaw |
Multicopter Control Derivative gain for YAW, values 0 - 200, default 60 |
fw_turn_assist_pitch_gain |
Gain required to keep constant pitch angle during coordinated turns (in TURN_ASSIST mode). Value significantly different from 1.0 indicates a problem with the airspeed calibration (if present) or value of fw_reference_airspeed parameter. Values 0 - 2, default 1 |
nav_mc_vel_xy_dterm_attenuation |
Maximum D-term attenution percentage for horizontal velocity PID controller (Multirotor). It allows to smooth the PosHold CRUISE, WP and RTH when Multirotor is traveling at full speed. Dterm is not attenuated at low speeds, breaking and accelerating. Values 0 - 100, default 90 |
nav_mc_vel_xy_dterm_attenuation_start |
A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins. Values 0 - 100, default 10 |
nav_mc_vel_xy_dterm_attenuation_end |
A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm _attenuation reaches maximum. Values 0-100, default 60 |
mc_cd_lpf_hz |
Cutoff frequency for Control Derivative. Lower value smoother reaction on fast stick movements. With higher values, response will be more aggressive and jerky. Values 0 - 200, default 30 |
setpoint_kalman_enabled |
Enable Kalman filter on the PID controller setpoint. Values OFF , ON , default OFF
|
setpoint_kalman_q |
Quality factor of the setpoint Kalman filter. Higher values means less filtering and lower phase delay. On 3-7 inch multirotors can be usually increased to 200-300 or even higher on clean builds. Values 1 - 16000, default 100 |
setpoint_kalman_w |
Window size for the setpoint Kalman filter. Wider the window, more samples are used to compute variance. In general, wider window results in smoother filter response. Values 1 - 40, default 4 |
setpoint_kalman_sharpness |
Dynamic factor for the setpoint Kalman filter. In general, the higher the value, the more dynamic Kalman filter gets. Values 1 - 16000, default 100 |
inav_use_gps_no_baro |
Values OFF , ON , default OFF
|
nav_fw_pitch2thr_smoothing |
How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by nav_fw_pitch2thr_threshold . Values 0 - 9, default 0 |
nav_fw_pitch2thr_threshold |
Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees]. Values 0 - 900, default 0 |
nav_fw_launch_end_time |
Time for the transition of throttle and pitch angle, between the launch state and the subsequent flight mode [ms]. Values 0 - 5000, default 2000 |
mavlink_extra3_rate |
Values 0 - 255, default 1 |
osd_snr_alarm |
Value below which Crossfire SNR Alarm pops-up. (dB). Values -12 - 8, default 4 |
osd_link_quality_alarm |
LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%". Values 0 - 100, default 70 |
osd_crsf_lq_format |
OSD display format for CRSF LQ. Values TYPE1 or TYPE2
|
osd_force_grid |
Force OSD to work in grid mode even if the OSD device supports pixel level access (mainly used for development). Default OFF
|
osd_ahi_bordered |
Shows a border/corners around the AHI region (pixel OSD only). Default OFF
|
osd_ahi_width |
AHI width in pixels (pixel OSD only). Values 0 - 255, default 132 |
osd_ahi_height |
AHI width in pixels (pixel OSD only). Values 0 - 255, default 162 |
osd_ahi_vertical_offset |
AHI vertical offset from center (pixel OSD only). Values -128 - 127, default 0 |
osd_sidebar_horizontal_offset |
Sidebar horizontal offset from default position. Positive values move the sidebars closer to the edges. Values -128 - 127, default 0 |
osd_left_sidebar_scroll_step |
How many units each sidebar step represents. 0 means the default value for the scroll type. Values 0 - 255, default 0 |
osd_right_sidebar_scroll_step |
How many units each sidebar step represents. 0 means the default value for the scroll type. Values 0 - 255, default 0 |
smartport_master_halfduplex |
Values OFF , ON , default ON
|
smartport_master_inverted |
Values OFF , ON , default OFF
|
dji_esc_temp_source |
Re-purpose the ESC temperature field for IMU/BARO temperature. Values ESC , IMU , BARO , default ESC
|
dji_workarounds |
Enables workarounds for different versions of MSP protocol used. Values 0 - 255, default 1. May be set to 0 for non-DJI rigs, otherwise leave at default. |
dji_use_name_for_messages |
Re-purpose the craft name field for messages. Replace craft name with :WTSED for Warnings, Throttle, Speed, Efficiency, Trip distance. Values OFF , ON , default ON
|
Setting | Description |
---|---|
nav_rth_home_offset_distance |
Replaced by safehome
|
nav_rth_home_offset_direction |
Replaced by safehome
|
gyro_notch1_hz and gyro_notch2_hz
|
Replaced by gyro_notch_hz
|
gyro_notch1_cutoff and gyro_notch2_cutoff
|
Replaced by gyro_notch_cutoff
|
use_dterm_fir_filter |
|
dterm_setpoint_weight |
|
dterm_notch_hz |
|
dterm_notch_cutoff |
|
mc_iterm_relax_type |
The SET_POI
WP type defines a location for a point of interest (POI). The craft will fly the mission (until a SET_HEAD) with the nose pointing at the POI, which might be useful for aerial photography. Note that the craft does NOT fly to the POI. Wiki description and example.
The SET_HEAD
type sets the craft's heading (where it 'looks', not the direction of travel). This may be useful for useful for aerial photography. A value of -1
causing the heading to be 'straight ahead', i.e. the direction of travel. Thus, SET_POI
-1
may used to cancel a previous valid SET_HEAD
or SET_POI
. A SET_HEAD
remains in force until cancelled by SET_HEAD
with p1
of -1
, or modified by a subsequent SET_HEAD
or SET_POI
. Wiki description and example.
For now, this new waypoint types works only for multirotors, as this type of aircraft can fly "looking" to a different direction than it's flying. Different of an airplane, which can only fly forward and thus can only look forward when flying.
Safehome replaces the nav_rth_home_offset_*
settings, and allows the pilot to define up to 8 alternative home locations as absolute positions (lat, lon as decimal degress * 10,000,000). If a safehome
is within 200m of the arming point, it will be used as the home location for RTH etc. Please see the separate document Safehomes.md.
WP mode activation with no mission loaded previously kept the current flight mode which may be counter-intuitive to the pilot. OSD will show that the mode is kept, however WP missions are generally not FPV. This PR creates a fallback in such case and will execute RTH instead which is safer than let the drone drift away. Also fixes a bug when RTH procedure may get interrupted in case of a brief sensor loss and switch out to ANGLE, ACRO or MANUAL instead of EMERGENCY. On airplanes with a certain RTH settings a brief GPS loss is tolerated in the navigation state machine, while the RTH activation bug would still bail out. This PR fixes this by making RTH procedure sticky, similar to other navigation flight modes.
inav 2.6 updates the build environment to use cmake
as the build management tool. The developer build documentation has been updated for all platforms (MacOS, Linux, Windows, FreeBSD). Please see the platform specific documentation.
inav 2.6 can populate warnings and multiple (by DJI unsupported) OSD elements into the craft_name field.
Enable the feature via set dji_use_name_for_messages = ON
and configure the elements through the name
, considering:
set name = :WDSTE
Published by digitalentity almost 4 years ago
Hello and welcome to INAV 2.6.0 Release Candidate 2!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
Compass has to be recalibrated. Do not import from previous INAV releases
Do not migrate Multirotor PID and filter settings from previous releases of INAV. Use Multirotor default preset (3"-7") instead and make required changes on top of that
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are deprecated and soon they will reach the end of support in INAV. If you are still using F3 boards, please migrate to F4 or F7.
INAV 2.6 will be the last release that supports F3-based boards. The supporting code will be retained for a few more releases, but will not be maintained and is not guarantee to build or work properly in future releases.
A new feature safehome
(see below) replaces nav_rth_home_offset_distance
and nav_rth_home_offset_direction
, offering a safer and much more flexible function. If you were using the nav_rth_home_offset_*
settings, please migrate to safehome
as these settings are removed.
Please follow the instructions on this page.
Command | Description |
---|---|
safehome |
List of home locations, see Safehomes.md and summary |
bind_rx |
Initiate binding for RX_SPI or SRXL2 receivers |
Setting | Description |
---|---|
mag_hardware |
New option added MSP
|
baro_hardware |
New options added DPS310 and MSP
|
pitot_hardware |
New options added MSP
|
serialrx_provider |
New options added FPORT2 and SRXL2
|
gps_provider |
New options added MSP
|
debug_mode |
New options added CD , KALMAN_GAIN , PID_MEASUREMENT , SPM_CELLS , SPM_VS600 , SPM_VARIO , PCF8574
|
airmode_type |
New option added STICK_CENTER_ONCE
|
nav_overrides_motor_stop |
Modified values OFF , AUTO_ONLY , ALL_NAV . When set OFF the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV. |
Setting | Description |
---|---|
gyro_notch_hz |
Replaces gyro_notch1_hz and gyro_notch2_hz
|
gyro_notch_cutoff |
Replaces gyro_notch1_cutoff and gyro_notch2_cutoff
|
maggain_x , maggain_y , maggain_z
|
Calibrated values replacing fixed values. Compass re-calibration is required. |
srxl2_unit_id |
Values 0 - 15, default 1 |
srxl2_baud_fast |
Values OFF , ON , default ON
|
mc_cd_pitch |
Multicopter Control Derivative gain for PITCH, values 0 - 200, default 60 |
mc_cd_roll |
Multicopter Control Derivative gain for ROLL, values 0 - 200, default 60 |
mc_cd_yaw |
Multicopter Control Derivative gain for YAW, values 0 - 200, default 60 |
fw_turn_assist_pitch_gain |
Gain required to keep constant pitch angle during coordinated turns (in TURN_ASSIST mode). Value significantly different from 1.0 indicates a problem with the airspeed calibration (if present) or value of fw_reference_airspeed parameter. Values 0 - 2, default 1 |
nav_mc_vel_xy_dterm_attenuation |
Maximum D-term attenution percentage for horizontal velocity PID controller (Multirotor). It allows to smooth the PosHold CRUISE, WP and RTH when Multirotor is traveling at full speed. Dterm is not attenuated at low speeds, breaking and accelerating. Values 0 - 100, default 90 |
nav_mc_vel_xy_dterm_attenuation_start |
A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins. Values 0 - 100, default 10 |
nav_mc_vel_xy_dterm_attenuation_end |
A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm _attenuation reaches maximum. Values 0-100, default 60 |
mc_cd_lpf_hz |
Cutoff frequency for Control Derivative. Lower value smoother reaction on fast stick movements. With higher values, response will be more aggressive and jerky. Values 0 - 200, default 30 |
setpoint_kalman_enabled |
Enable Kalman filter on the PID controller setpoint. Values OFF , ON , default OFF
|
setpoint_kalman_q |
Quality factor of the setpoint Kalman filter. Higher values means less filtering and lower phase delay. On 3-7 inch multirotors can be usually increased to 200-300 or even higher on clean builds. Values 1 - 16000, default 100 |
setpoint_kalman_w |
Window size for the setpoint Kalman filter. Wider the window, more samples are used to compute variance. In general, wider window results in smoother filter response. Values 1 - 40, default 4 |
setpoint_kalman_sharpness |
Dynamic factor for the setpoint Kalman filter. In general, the higher the value, the more dynamic Kalman filter gets. Values 1 - 16000, default 100 |
inav_use_gps_no_baro |
Values OFF , ON , default OFF
|
nav_fw_pitch2thr_smoothing |
How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by nav_fw_pitch2thr_threshold . Values 0 - 9, default 0 |
nav_fw_pitch2thr_threshold |
Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees]. Values 0 - 900, default 0 |
nav_fw_launch_end_time |
Time for the transition of throttle and pitch angle, between the launch state and the subsequent flight mode [ms]. Values 0 - 5000, default 2000 |
mavlink_extra3_rate |
Values 0 - 255, default 1 |
osd_snr_alarm |
Value below which Crossfire SNR Alarm pops-up. (dB). Values -12 - 8, default 4 |
osd_link_quality_alarm |
LQ % indicator blinks below this value. For Crossfire use 70%, for Tracer use 50%". Values 0 - 100, default 70 |
osd_crsf_lq_format |
OSD display format for CRSF LQ. Values TYPE1 or TYPE2
|
osd_force_grid |
Force OSD to work in grid mode even if the OSD device supports pixel level access (mainly used for development). Default OFF
|
osd_ahi_bordered |
Shows a border/corners around the AHI region (pixel OSD only). Default OFF
|
osd_ahi_width |
AHI width in pixels (pixel OSD only). Values 0 - 255, default 132 |
osd_ahi_height |
AHI width in pixels (pixel OSD only). Values 0 - 255, default 162 |
osd_ahi_vertical_offset |
AHI vertical offset from center (pixel OSD only). Values -128 - 127, default 0 |
osd_sidebar_horizontal_offset |
Sidebar horizontal offset from default position. Positive values move the sidebars closer to the edges. Values -128 - 127, default 0 |
osd_left_sidebar_scroll_step |
How many units each sidebar step represents. 0 means the default value for the scroll type. Values 0 - 255, default 0 |
osd_right_sidebar_scroll_step |
How many units each sidebar step represents. 0 means the default value for the scroll type. Values 0 - 255, default 0 |
smartport_master_halfduplex |
Values OFF , ON , default ON
|
smartport_master_inverted |
Values OFF , ON , default OFF
|
dji_esc_temp_source |
Re-purpose the ESC temperature field for IMU/BARO temperature. Values ESC , IMU , BARO , default ESC
|
dji_workarounds |
Enables workarounds for different versions of MSP protocol used. Values 0 - 255, default 1. May be set to 0 for non-DJI rigs, otherwise leave at default. |
dji_use_name_for_messages |
Re-purpose the craft name field for messages. Replace craft name with :WTSED for Warnings, Throttle, Speed, Efficiency, Trip distance. Values OFF , ON , default ON
|
Setting | Description |
---|---|
nav_rth_home_offset_distance |
Replaced by safehome
|
nav_rth_home_offset_direction |
Replaced by safehome
|
gyro_notch1_hz and gyro_notch2_hz
|
Replaced by gyro_notch_hz
|
gyro_notch1_cutoff and gyro_notch2_cutoff
|
Replaced by gyro_notch_cutoff
|
use_dterm_fir_filter |
|
dterm_setpoint_weight |
|
dterm_notch_hz |
|
dterm_notch_cutoff |
|
mc_iterm_relax_type |
The SET_POI
WP type defines a location for a point of interest (POI). The craft will fly the mission (until a SET_HEAD) with the nose pointing at the POI, which might be useful for aerial photography. Note that the craft does NOT fly to the POI. Wiki description and example.
The SET_HEAD
type sets the craft's heading (where it 'looks', not the direction of travel). This may be useful for useful for aerial photography. A value of -1
causing the heading to be 'straight ahead', i.e. the direction of travel. Thus, SET_POI
-1
may used to cancel a previous valid SET_HEAD
or SET_POI
. A SET_HEAD
remains in force until cancelled by SET_HEAD
with p1
of -1
, or modified by a subsequent SET_HEAD
or SET_POI
. Wiki description and example.
For now, this new waypoint types works only for multirotors, as this type of aircraft can fly "looking" to a different direction than it's flying. Different of an airplane, which can only fly forward and thus can only look forward when flying.
Safehome replaces the nav_rth_home_offset_*
settings, and allows the pilot to define up to 8 alternative home locations as absolute positions (lat, lon as decimal degress * 10,000,000). If a safehome
is within 200m of the arming point, it will be used as the home location for RTH etc. Please see the separate document Safehomes.md.
WP mode activation with no mission loaded previously kept the current flight mode which may be counter-intuitive to the pilot. OSD will show that the mode is kept, however WP missions are generally not FPV. This PR creates a fallback in such case and will execute RTH instead which is safer than let the drone drift away. Also fixes a bug when RTH procedure may get interrupted in case of a brief sensor loss and switch out to ANGLE, ACRO or MANUAL instead of EMERGENCY. On airplanes with a certain RTH settings a brief GPS loss is tolerated in the navigation state machine, while the RTH activation bug would still bail out. This PR fixes this by making RTH procedure sticky, similar to other navigation flight modes.
inav 2.6 updates the build environment to use cmake
as the build management tool. The developer build documentation has been updated for all platforms (MacOS, Linux, Windows, FreeBSD). Please see the platform specific documentation.
inav 2.6 can populate warnings and multiple (by DJI unsupported) OSD elements into the craft_name field.
Enable the feature via set dji_use_name_for_messages = ON
and configure the elements through the name
, considering:
set name = :WDSTE
Published by digitalentity about 4 years ago
Hello and welcome to INAV 2.5.2 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
This is a patch release with support for several new targets and a few bugfixes.
Published by digitalentity over 4 years ago
Hello and welcome to INAV 2.5.1 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
This is a bug-fix release. Notable changes:
Since 2.5.1 TRAMP protocol detects max power that VTX is reporting and caps the max setting to that power. Some VTXes don't report that properly. A new CLI setting vtx_max_power_override
allows to set the max power manually in such cases. Use caution!
Due to a regression bug in 2.5.0 DSHOT ESC telemetry was not working. This is now fixed.
Legacy condition that limited VTX updates to unarmed state only is now removed. VTX settings changes in flight are now working reliably.
Published by digitalentity over 4 years ago
Hello and welcome to INAV 2.5.0 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
aux
mode migrationinav 2.5 moves the CLI aux
mode value from a boxid
that was not guaranteed to be stable between releases to a permmanentId
that is guaranteed to be stable between releases. This is a "breaking" change for inav 2.5 that brings stability in the future.
In order to use a diff
or dump
from 2.4 or earlier in inav 2.5, the user must do one of the following:
aux
settings from the diff
/ dump
and recreate them in inav 2.5; ordiff
/ dump
automatically; oraux
settings; a conversion table is provided as part of the box2perm documentation.All traces of PWM
RX have finally been removed. Please check that your receiver type is correctly assigned before raising bogus issues that your RX no longer works.
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are deprecated and soon they will reach the end of support in INAV. If you are still using F3 boards, please migrate to F4 or F7.
diff
to update or remove the aux
statementsPlease follow the instructions on this page.
Command | Description |
---|---|
gf |
Global Functions. For details refer to Global Functions.md in the docs folder. |
logic |
Defined Logic conditions activating Global Functions. For details refer to Logic Conditions.md in the docs folder. |
Setting | Description |
---|---|
dynamic_gyro_notch_enabled |
Enable/disable dynamic gyro notch also known as Matrix Filter [ON / OFF] |
dynamic_gyro_notch_range |
Range for dynamic gyro notches. MEDIUM for 5", HIGH for 3" and MEDIUM or LOW for 7" and bigger propellers |
dynamic_gyro_notch_q |
Q factor for dynamic notches |
dynamic_gyro_notch_min_hz |
Minimum frequency for dynamic notches. Default value of 150 works best with 5" multirors. Should be lowered with increased size of propellers. Values around 100 work fine on 7" drones. 10" can go down to 60 - 70 |
motor_direction_inverted |
Replaces yaw_motor_direction
|
nav_fw_control_smoothness |
Controls smoothness of navigation control (0-9). 0 gives legacy behaviour, non-zero values give increasing smoothness. |
nav_fw_pos_hdg_p |
P gain of heading PID controller. |
nav_fw_pos_hdg_i |
I gain of heading PID controller. |
nav_fw_pos_hdg_d |
D gain of heading PID controller. |
nav_fw_pos_hdg_pidsum_limit |
Output limit for heading trajectory PID controller. (Fixedwing, rovers, boats) |
nav_use_fw_yaw_control |
Enables or Disables the use of the heading PID controller on fixed wing |
nav_fw_yaw_deadband |
Deadband for heading trajectory PID controller. When heading error is below the deadband, controller assumes that vehicle is on course |
osd_esc_temp_alarm_max |
Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade) |
osd_esc_temp_alarm_min |
Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade) |
osd_hud_wp_disp |
Controls display of the next waypoints in the HUD. See description below |
osd_ahi_style |
Sets OSD Artificial Horizon style "DEFAULT" or "LINE" for the FrSky Graphical OSD |
telemetry_halfduplex |
Replaces telemetry_uart_unidir
|
servo_protocol |
Select which protocol is used to communicate with servos (PWM, servo driver or SBUS) |
Setting | Description |
---|---|
dyn_notch_width_percent |
|
dyn_notch_range |
|
dyn_notch_q |
|
dyn_notch_min_hz |
|
rpm_dterm_filter_enabled |
|
dterm_gyro_harmonic |
|
rpm_dterm_min_hz |
|
rpm_dterm_q |
|
telemetry_uart_unidir |
Replaced by telemetry_halfduplex
|
yaw_motor_direction |
Replaced by motor_direction_inverted
|
Starting from version 2.5, INAV supports Rovers and Boats (more general: ground and water vehicles without altitude control with yaw steering only. Remark: tanks and vehicles with differential steering are also supported).
The Rover and Boat related features:
Description
The new Matrix Notch filter comes enabled by default on INAV. It's a dynamic notch filter that detects noise frequencies on each individual axis (X, Y and Z) and apply the filters to each axis, resulting in a much better noise handling.
Check out this video to see a detailed explanation of how the Matrix Filter works.
INAV 2.5 supports additional waypoint types, allowing more complex missions to be performed.
The navigation messages wiki page provides more information and annotated examples.
Shows the next waypoints in the hud. To enable this feature, enter the count of next waypoints in the CLI command:
set osd_hud_wp_disp = 0 to 3
Or on the CMS menu: OSD > HUD > Displayed items > Next waypoints: (from 0 to 3, 0 means disabled)
Then start a WP mission, the next WPs will appear as soon as the mission is loaded in FC memory AND that the aircraft has a valid GPS heading, so it must move if it's not fitted with a magnetometer.
It's now possible to connect S.BUS servos to INAV. You can configure INAV to output servo commands as S.BUS stream on one of the serial ports. Important note - F4 boards generally don't support inversion on serial ports, for those boards a hardware inverter might be required.
Now CMS has one unified page for configuring VTX settings. No need to remember which protocol your VTX is talking (Tramp, S.Audio or other).
ESC sensor can now be put to listen-only mode, allowing ESC sensor functionality to be used when an ESC is connected with a PWM-based protocol and configured to sent telemetry automatically. This will be useful on airplanes to provide RPM feedback without the need to use DSHOT.
Due to flash / memory restrictions the following functions have been disabled on F3 targets:
You can get more suggestions following this link too.
Published by digitalentity over 4 years ago
Hello and welcome to INAV 2.5.0 Release!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
aux
mode migrationinav 2.5 moves the CLI aux
mode value from a boxid
that was not guaranteed to be stable between releases to a permmanentId
that is guaranteed to be stable between releases. This is a "breaking" change for inav 2.5 that brings stability in the future.
In order to use a diff
or dump
from 2.4 or earlier in INAV 2.5, the user must do one of the following:
aux
settings from the diff
/ dump
and recreate them in INAV 2.5; ordiff
/ dump
automatically; ordiff
for INAV 2.5aux
settings; a conversion table is provided as part of the box2perm documentation.All traces of PWM
RX have finally been removed. Please check that your receiver type is correctly assigned before raising bogus issues that your RX no longer works.
STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are deprecated and soon they will reach the end of support in INAV. If you are still using F3 boards, please migrate to F4 or F7.
diff
to update or remove the aux
statementsPlease follow the instructions on this page.
Command | Description |
---|---|
gf |
Global Functions. For details refer to Global Functions.md in the docs folder. |
logic |
Defined Logic conditions activating Global Functions. For details refer to Logic Conditions.md in the docs folder. |
Setting | Description |
---|---|
dynamic_gyro_notch_enabled |
Enable/disable dynamic gyro notch also known as Matrix Filter [ON / OFF] |
dynamic_gyro_notch_range |
Range for dynamic gyro notches. MEDIUM for 5", HIGH for 3" and MEDIUM or LOW for 7" and bigger propellers |
dynamic_gyro_notch_q |
Q factor for dynamic notches |
dynamic_gyro_notch_min_hz |
Minimum frequency for dynamic notches. Default value of 150 works best with 5" multirors. Should be lowered with increased size of propellers. Values around 100 work fine on 7" drones. 10" can go down to 60 - 70 |
motor_direction_inverted |
Replaces yaw_motor_direction
|
nav_fw_control_smoothness |
Controls smoothness of navigation control (0-9). 0 gives legacy behaviour, non-zero values give increasing smoothness. |
nav_fw_pos_hdg_p |
P gain of heading PID controller. |
nav_fw_pos_hdg_i |
I gain of heading PID controller. |
nav_fw_pos_hdg_d |
D gain of heading PID controller. |
nav_fw_pos_hdg_pidsum_limit |
Output limit for heading trajectory PID controller. (Fixedwing, rovers, boats) |
nav_use_fw_yaw_control |
Enables or Disables the use of the heading PID controller on fixed wing |
nav_fw_yaw_deadband |
Deadband for heading trajectory PID controller. When heading error is below the deadband, controller assumes that vehicle is on course |
osd_esc_temp_alarm_max |
Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade) |
osd_esc_temp_alarm_min |
Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade) |
osd_hud_wp_disp |
Controls display of the next waypoints in the HUD. See description below |
osd_ahi_style |
Sets OSD Artificial Horizon style "DEFAULT" or "LINE" for the FrSky Graphical OSD |
telemetry_halfduplex |
Replaces telemetry_uart_unidir
|
servo_protocol |
Select which protocol is used to communicate with servos (PWM, servo driver or SBUS) |
Setting | Description |
---|---|
dyn_notch_width_percent |
|
dyn_notch_range |
|
dyn_notch_q |
|
dyn_notch_min_hz |
|
rpm_dterm_filter_enabled |
|
dterm_gyro_harmonic |
|
rpm_dterm_min_hz |
|
rpm_dterm_q |
|
telemetry_uart_unidir |
Replaced by telemetry_halfduplex
|
yaw_motor_direction |
Replaced by motor_direction_inverted
|
Starting from version 2.5, INAV supports Rovers and Boats (more general: ground and water vehicles without altitude control with yaw steering only. Remark: tanks and vehicles with differential steering are also supported).
The Rover and Boat related features:
Description
The new Matrix Notch filter comes enabled by default on INAV. It's a dynamic notch filter that detects noise frequencies on each individual axis (X, Y and Z) and apply the filters to each axis, resulting in a much better noise handling.
Check out this video to see a detailed explanation of how the Matrix Filter works.
INAV 2.5 supports additional waypoint types, allowing more complex missions to be performed.
The navigation messages wiki page provides more information and annotated examples.
Shows the next waypoints in the hud. To enable this feature, enter the count of next waypoints in the CLI command:
set osd_hud_wp_disp = 0 to 3
Or on the CMS menu: OSD > HUD > Displayed items > Next waypoints: (from 0 to 3, 0 means disabled)
Then start a WP mission, the next WPs will appear as soon as the mission is loaded in FC memory AND that the aircraft has a valid GPS heading, so it must move if it's not fitted with a magnetometer.
It's now possible to connect S.BUS servos to INAV. You can configure INAV to output servo commands as S.BUS stream on one of the serial ports. Important note - F4 boards generally don't support inversion on serial ports, for those boards a hardware inverter might be required.
Now CMS has one unified page for configuring VTX settings. No need to remember which protocol your VTX is talking (Tramp, S.Audio or other).
ESC sensor can now be put to listen-only mode, allowing ESC sensor functionality to be used when an ESC is connected with a PWM-based protocol and configured to sent telemetry automatically. This will be useful on airplanes to provide RPM feedback without the need to use DSHOT.
Due to flash / memory restrictions the following functions have been disabled on F3 targets:
Published by digitalentity over 4 years ago
Hello and welcome to INAV 2.5.0 RC1!
Please carefully read all of this document for the best possible experience and safety.
Get in touch with other pilots, share experiences, suggestions and ask for help on:
Please continue to support developers, for free, by checking out from the following stores after having clicked on the following links:
Your contribution from the past month has been very welcome! Thanks!
Tested and suggested hardware can be found here
aux
mode migrationinav 2.5 moves the CLI aux
mode value from a boxid
that was not guaranteed to be stable between releases to a permmanentId
that is guaranteed to be stable between releases. This is a "breaking" change for inav 2.5 that brings stability in the future.
In order to use a diff
or dump
from 2.4 or earlier in inav 2.5, the user must do one of the following:
aux
settings from the diff
/ dump
and recreate them in inav 2.5; ordiff
/ dump
automatically; oraux
settings; a conversion table is provided as part of the box2perm documentation.STM32 F3 flight controllers like Omnibus F3 or SP Racing F3 are deprecated and soon they will reach the end of support in INAV. If you are still using F3 boards, please migrate to F4 or F7.
diff
to update or remove the aux
statementsPlease follow the instructions on this page.
Command | Description |
---|---|
gf |
Global Functions. For details refer to Global Functions.md in the docs folder. |
logic |
Defined Logic conditions activating Global Functions. For details refer to Logic Conditions.md in the docs folder. |
Setting | Description |
---|---|
dynamic_gyro_notch_enabled |
Enable/disable dynamic gyro notch also known as Matrix Filter [ON / OFF] |
dynamic_gyro_notch_range |
Range for dynamic gyro notches. MEDIUM for 5", HIGH for 3" and MEDIUM or LOW for 7" and bigger propellers |
dynamic_gyro_notch_q |
Q factor for dynamic notches |
dynamic_gyro_notch_min_hz |
Minimum frequency for dynamic notches. Default value of 150 works best with 5" multirors. Should be lowered with increased size of propellers. Values around 100 work fine on 7" drones. 10" can go down to 60 - 70 |
motor_direction_inverted |
Cli.md UPDATE Boolean ON / OFF, replaces yaw_motor_direction
|
nav_fw_pos_hdg_p |
Cli.md MISSING |
nav_fw_pos_hdg_i |
Cli.md MISSING |
nav_fw_pos_hdg_d |
Cli.md MISSING |
nav_fw_pos_hdg_pidsum_limit |
Cli.md MISSING |
nav_use_fw_yaw_control |
Cli.md MISSING |
nav_fw_yaw_deadband |
Cli.md MISSING |
osd_esc_temp_alarm_max |
Temperature under which the IMU temperature OSD element will start blinking (decidegrees centigrade) |
osd_esc_temp_alarm_min |
Temperature above which the IMU temperature OSD element will start blinking (decidegrees centigrade) |
osd_hud_wp_disp |
Cli.md MISSING Controls display of the next waypoints in the HUD. See description below |
osd_ahi_style |
Cli.md MISSING Sets OSD Artificial Horizon style "DEFAULT" or "LINE" |
telemetry_halfduplex |
Cli.md UPDATE Replaces telemetry_uart_unidir
|
servo_protocol |
Select which protocol is used to communicate with servos (PWM, servo driver or SBUS) |
Setting | Description |
---|---|
dyn_notch_width_percent |
|
dyn_notch_range |
|
dyn_notch_q |
|
dyn_notch_min_hz |
|
rpm_dterm_filter_enabled |
|
dterm_gyro_harmonic |
|
rpm_dterm_min_hz |
|
rpm_dterm_q |
|
telemetry_uart_unidir |
Cli.md UPDATE Replaced by telemetry_halfduplex
|
yaw_motor_direction |
Cli.md UPDATE Replaced by motor_direction_inverted
|
Starting from version 2.5, INAV supports Rovers and Boats (more general: ground and water vehicles without altitude control with yaw steering only. Remark: tanks and vehicles with differential steering are also supported).
The Rover and Boat related features:
Description
The new Matrix Notch filter comes enabled by default on INAV. It's a dynamic notch filter that detects noise frequencies on each individual axis (X, Y and Z) and apply the filters to each axis, resulting in a much better noise handling.
Check out this video to see a detailed explanation of how the Matrix Filter works.
INAV 2.5 supports additional waypoint types, allowing more complex missions to be performed.
The navigation messages wiki page provides more information and annotated examples.
Shows the next waypoints in the hud. To enable this feature, enter the count of next waypoints in the CLI command:
set osd_hud_wp_disp = 0 to 3
Or on the CMS menu: OSD > HUD > Displayed items > Next waypoints: (from 0 to 3, 0 means disabled)
Then start a WP mission, the next WPs will appear as soon as the mission is loaded in FC memory AND that the aircraft has a valid GPS heading, so it must move if it's not fitted with a magnetometer.
It's now possible to connect S.BUS servos to INAV. You can configure INAV to output servo commands as S.BUS stream on one of the serial ports. Important note - F4 boards generally don't support inversion on serial ports, for those boards a hardware inverter might be required.
Now CMS has one unified page for configuring VTX settings. No need to remember which protocol your VTX is talking (Tramp, S.Audio or other).
ESC sensor can now be put to listen-only mode, allowing ESC sensor functionality to be used when an ESC is connected with a PWM-based protocol and configured to sent telemetry automatically. This will be useful on airplanes to provide RPM feedback without the need to use DSHOT.
Due to flash / memory restrictions the following functions have been disabled on F3 targets: