- 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>
Unfortunately this commit contains two things:
1. Some cleanup and renaiming.
2. An additional wait until lockstep has been initialized.
By waiting until HIL_SENSOR messages arrive including timestamps we
stop the startup script and prevent other modules from running until
time is set up. This should resolve some busy waiting by various
modules and prevent races on initialization (e.g. the landing state
being subscribed by mavlink before being published by the land
detector).
The previous boot configuration took at minimum one second to boot. This is in particular significant in tests when the system is often started and stopped
The test was testing the result of 3D float vector operations with binary equality of the floating point numbers, which is not a valid assumption to make for floating point math. This change switches to proper comparisons with float accuracy and compares vectors using the norm of their difference.
