This caused bad altitude control performance when enabling
terrain following. It even leads to complete vertical control
instability in case dist_bottom is inaccurate.
Relying on the estimator states is the way to go instead of
silently using one altitude source as state.
- split out integrated data into new standalone messages (sensor_accel_integrated and sensor_gyro_integrated)
- publish sensor_gyro at full rate and remove sensor_gyro_control
- limit sensor status publications to 10 Hz
- remove unused accel/gyro raw ADC fields
- add device IDs to sensor_bias and sensor_correction
- vehicle_angular_velocity/vehicle_acceleration: check device ids before using bias and corrections
* Treat UAVS diffrently from manned aviation
* Added fake_traffic testing functionality,
* Added NAV_TRAFF_AVOID Hold and Landmode
* Added Behavior: HOLD Position to collision avoidance mode and implemented Landmode to collision avoidance.
Boards where no Hardware GUID is defined will send 0 as GUID.
Right now collision avoidance for more than one FMU without Hardware GUID is not possible.
We should consider adding a randomly generated HW GUID as a placeholder for legacy Boards
The bulk of this change was tightly coupled and needed to be deleted in one pass. Some of the smaller changes were things that broke as a result of the initial purge and subsequently fixed by further eradicating unnecessary platform differences. Finally, I deleted any dead code I came across in the related files I touched while going through everything.
- DriverFramework (src/lib/DriverFramework submodule) completely removed
- added dspal submodule in qurt platform (was brought in via DriverFramework)
- all df wrapper drivers removed
- all boards using df wrapper drivers updated to use in tree equivalents
- unused empty arch/board.h on posix and qurt removed
- unused IOCTLs removed (pub block, priv, etc)
- Integrator delete methods only used from df wrapper drivers
- commander: sensor calibration use "NuttX version" everywhere for now
- sensors: update to px4_{open, read, close} instead of DevMgr wrapper (adc open for analog differential pressure)
- battery_status: update to px4_{open, read, close} instead of DevMgr wrapper (adc open for analog differential pressure)
- cdev cleanup conflicting typedefs and names with actual OS (pollevent_t, etc)
- load_mon and top remove from linux boards (unused)
- delete unused PX4_MAIN_FUNCTION
- delete unused getreg32 macro
- delete unused SIOCDEVPRIVATE define
- named each platform tasks consistently
- posix list_devices and list_topics removed (list_files now shows all virtual files)
- this is one of the last pieces of the system that still depend on DriverFramework
- add new SIM_GPS_NOISE_X parameter for optionally increasing the GPS noise multiplier (was previously a gpssim command line option)
- add SIM_x_BLOCK parameters to block sensor publication
- SIM_GPS_BLOCK
- SIM_ACCEL_BLOCK
- SIM_GYRO_BLOCK
- SIM_MAG_BLOCK
- SIM_BARO_BLOCK
- SIM_DPRES_BLOCK
* parameter and logic to commander for triggering failsafe from external automatic trigger system.
* logic to startup script for enabling ATS. Added uORB publishing to pwm_input module.
* Refactored out CDev usage from pwm_input and ll40ls. Refactored out ll40ls specifics from pwm_input and cleaned up dead code.
* NotchFilter: add NotchFilter template and test for float type
* NotchFilterTest: add test for Vector3f notch filter
* PX4Gyroscope: add notch filter with IMU_GYRO_NF_(FREQ|BW) parameters to
set the notch center frequency and bandwidth
Innovation ratios have no unit: it is a ratio of to squared base unit.
For example:
[COM_ARM_EKF_VEL] = [vel_innov]**2 / ([GATE_SIZE]**2 * [VEL_VAR])
= [m/s]**2 / ([1]**2 * [m/s]**2)
= [1]
- deprecate DriverFramework bmp280 driver (df_bmp280_wrapper)
- update beaglebone blue and snapdragon flight eagle boards to use in tree bmp280
- update posix (really just linux) and qurt I2C wrappers
- tested on beaglebone blue
* Mavlink: subscribe to airspeed_validated instead of airspeed topic
This e.g. changes the way QGC displays the airspeed in case of an
airspeed failure (0 instead of the last valid airspeed). It will
always display the airspeed that's used currently in the control
modules.
* FW land detector: move to subscribe to airspeed_validated instead of airspeed topic
- the land detector checks further if the airspeed is NAN, in which case
it sets the airspeed to 0 (min groundspeed, vz and accel checks still
have to pass.
* Fixed-wing land detector use airspeed_vaidated: addressed review comments
- replaced ternary by conditional
- set airspeed to 0 if airspeed_validated stops publishing
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- rename of flag in position sp: from allow_weather_vane to disable_weather_vane
- flag now doesn't have to be set for all auto modes, meaning that weather vane is also active outside of mission
- flag is set before front transition to align with wp, and unset after alignment is over
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Matthias Grob