In a velocity reset we only used the GPS measurement if _gps_check_fail_status.value was equal to zero. The value of this flag is independent of EKF2_GPS_CHECK so checks can fail even if they are not configured to have any effect.
This fixes SITL with lockstep when using LPE and q estimator.
The required changes are:
- Publish ekf2_timestamps because simulator_mavlink expects them.
- Run LPE at 250 Hz instead of 80 Hz in order to keep everything in
lockstep running at 250 Hz.
- this is disabled in replay builds to ensure all data in ekf2 replay logs only contains the same time range, otherwise the plots can be unreadable using common tools
- fixes#14230
* 8 kHz gyro, 4 kHz accel
* DLPF disabled
* scheduled using data ready interrupts
* FIFO is emptied at 1 kHz by default, but can adjusted via IMU_GYRO_RATEMAX from 250 Hz - 2000 kHz.
* On both px4_fmu-v4 and px4_fmu-v4pro the secondary IMU is an mpu9250 with the same driver
- refactor Run() into simple state machine
- perform reset and configuration in sensor bus thread
- when using data ready interrupt skip checking FIFO count
- fix periodic temperature sampling (rate limit to 1 Hz)
- refactor Run() into simple state machine
- perform reset and configuration in sensor bus thread
- when using data ready interrupt skip checking FIFO count
- fix periodic temperature sampling (rate limit to 1 Hz)
- refactor Run() into simple state machine
- perform reset and configuration in sensor bus thread
- when using data ready interrupt skip checking FIFO count
- fix periodic temperature sampling (rate limit to 1 Hz)
- refactor Run() into simple state machine
- perform reset and configuration in sensor bus thread
- when using data ready interrupt skip checking FIFO count
Sometimes in CI for VTOL we saw disarms before the spoolup and ramp were
over and the takeoff would actually happen. By raising the auto-disarm
time we should be able to work around this and get CI less flaky.
* Introduce "px4_arch_adc_reference_v"
* Revert "Introduce "px4_arch_adc_reference_v""
This reverts commit 93691fbbd55a1b8da8c190e225b318067d90399b.
* use structure to return sample count and vref at the same time
* Revert "use structure to return sample count and vref at the same time"
This reverts commit 9cfd1c173cda51495f766a3f678c2202d67725fd.
* Revert "Revert "Introduce "px4_arch_adc_reference_v"""
This reverts commit edb7f7603e4471163ffb0fc6fc62ad2e30336e91.
* fix missed reference
* remove unecessary channel specific vref
* Update src/drivers/drv_adc.h
Co-Authored-By: David Sidrane <David.Sidrane@Nscdg.com>
* Update src/drivers/drv_adc.h
Co-Authored-By: David Sidrane <David.Sidrane@Nscdg.com>
* Introduce BOARD_ADC_POS_REF_V
Co-authored-by: David Sidrane <David.Sidrane@Nscdg.com>
To obtain the correct difference between two angles, we need to wrap
the result between -pi and pi. Otherwise, the difference between two
angles close to 180 degrees but with opposite signs will produce a large
error.
For example if a = -179 and b = 179, b - a = 258 instead of -2 degrees
Regression from https://github.com/PX4/Firmware/pull/13613.
VEHICLE_CMD_COMPONENT_ARM_DISARM from CLI would enter the
ARMING_STATE_IN_AIR_RESTORE logic. This was never intended for disarming
(and leads to state machine transition failures), and IMO it is also not
intended for commands from CLI.
Lorenz Meier