* PreFlightCheck: remove unused reportFailures flag
* Commander: pull all pre flight checks together on the PreFlightCheck class
* PreFlightCheck: separate checks into their own files
This fixes the case where the mixer_module would subscribe and use its
own test_motor publication which was created only to make sure the
topic is advertised and subsequent updates will work properly.
This happened in SITL lockstep because the timestamp would be 0 at the
very beginning, and hence elapsed time would be 0 as well.
This lead to an actuator publication which would then get lockstep out
of sync causing poll errors on the Gazebo side.
* Use position instead of last setpoint
This calculates the target velocities better taking into account disturbances along
the flight route. Previously entry angles and more were calculated assuming the flight path
originates directly from the direction of the previous waypoint. This corrects this assumption
to instead make the direction come from the vehicle location.
* Allow to specify a final speed given a braking distance.
This is to allow planning to not stop at a waypoint, but instead
to reach the waypoint while maintaining a certain velocity
* Updated src/lib/matrix
* Account for speed at target when determining constraints
* Separate constraints into x/y components
* Use setpoint position, not vehicle position
* Fix whitespace, add documentation
and remove the px4_ prefix, except for px4_config.h.
command to update includes:
for k in app.h atomic.h cli.h console_buffer.h defines.h getopt.h i2c.h init.h log.h micro_hal.h module.h module_params.h param.h param_macros.h posix.h sem.h sem.hpp shmem.h shutdown.h tasks.h time.h workqueue.h; do for i in $(grep -rl 'include <px4_'$k src platforms boards); do sed -i 's/#include <px4_'$k'/#include <px4_platform_common\/'$k/ $i; done; done
for in $(grep -rl 'include <px4_config.h' src platforms boards); do sed -i 's/#include <px4_config.h/#include <px4_platform_common\/px4_config.h'/ $i; done
Transitional headers for submodules are added (px4_{defines,log,time}.h)
- move most orb to uORB::Publication and uORB::Subscription
- update legacy message handling (warn to PX4_INFO, PX4_WARN, PX4_ERR)
- add perf counters
- sensors/mag support newer `uavcan::equipment::ahrs::MagneticFieldStrength2` message
- sensors/gps support `uavcan::equipment::gnss::Auxiliary` for hdop and vdop
- sensors delete obsolete ioctl and read methods
- use PublicationMulti for actuator_outputs and esc_reports (to coexist with other output modules)
- add GNSS parameter metadata (parameters_injected.xml)
- ecl in PX4/Firmware (dcfe226638): https://github.com/PX4/ecl/commit/f005e0ea8f33d10dd014a0700e712426540bb58a
- ecl current upstream: https://github.com/PX4/ecl/commit/9b4b24ee71902c6a4289170e8fb1ca3306c1d9c4
- Changes: https://github.com/PX4/ecl/compare/f005e0ea8f33d10dd014a0700e712426540bb58a...9b4b24ee71902c6a4289170e8fb1ca3306c1d9c49b4b24e 2019-10-17 RomanBapst - removed unused definition
0e3a0b8 2019-10-15 RomanBapst - range_finder_checks: parametrised signal quality hysteresis duration
16d1e15 2019-10-15 RomanBapst - addressed review comments
6bc6f26 2019-10-14 RomanBapst - range_finder_checks: set range height to valid if signal quality is non-zero
6299d81 2019-10-14 RomanBapst - ekf_helper: use latest validated range sample to reset height
00f49e6 2019-10-14 RomanBapst - cleanup checks of range finder data
4d37065 2019-08-22 Paul Riseborough - EKF: Make use of inverse rotation function consistent with name
36de2b3 2019-08-22 Paul Riseborough - EKF: Use matrix library for quaternion to rotation matrix conversion
1a4ab06 2019-10-22 bresch - rate controller: add override specifiers whenever needed
29f71ff 2019-10-21 bresch - ekf: Add override specifier for all functions that override virtual functions of the estimator interface class
50167bf 2019-10-16 bresch - estimator interface: add deprecated functions for backward compatibility
b38458c 2019-10-10 bresch - Terrain estimator: formatting and remove redundant comments
0aef0ed 2019-10-10 bresch - terrain_estimator: remove dead code. Since the terrain estimator is constantly reset on ground, it is not necessary anymore to fuse fake measurements on ground if the range measurements are bad.
370e04e 2019-10-03 bresch - terrain_est: Continuously reset terrain height on ground using known clearance. This is the best estimate as we should not rely on a distance sensor while on the ground. This also helps when the drone is carried over as it avoids starting with a crazy downward distance for optical flow scaling.
e09e3e1 2019-10-14 bresch - control: rename _range_aid_enabled to _is_range_aid_suitable rename rangeAidConditionsMet to checkRangeAidSuitability
fac69d0 2019-10-14 bresch - control: refactor rangeAidConditionsMet function
eae6e8f 2019-08-06 Paul Riseborough - EKF: Fix on ground yaw drift when using EKF2_MAG_TYPE = 4
4e946d5 2019-09-04 RomanBapst - implemented synthesized magnetometer Z measurement - calculate a theoretical value based on the knowledge of the direction and strength of the magnetic field vector and X/Y sensor measurements - needs knowledge about location on earth to work
The constrainAbs function was not prioritizing the minimum value
that produces the autocontinue behaviour. This caused zig-zag
paths when the waypoints were almost -but not exactly- aligned.
Some of these perf counters were useful during initial development, but realistically aren't needed anymore, some are redundant when we can now see the average interval from `work_queue status` and some of them simply aren't worth the cost at higher rates.
Required for pwm_out_sim: only publish actuator_outputs when we get
actuator_controls. Otherwise lockstep startup does not work.
The issue was there before but hidden, due to a long poll timeout.
Works with HIL too.
Checking the first output_limited for a disarmed value is fragile.
For example a disarmed value might be within the range of min/max output
values and could then be triggered while armed.
This adds a flight task to catch the case where we want to do an
emergency descent without GPS but only a baro.
Previously, this would lead to the navigator land class being called
without position estimates which then made the flight tasks fail and
react with a flight task failsafe. This however meant that landed was
never detected and a couple of confusing error messages.
This applies if NAV_RCL_ACT is set to 3 "land".
* rename parameters to allow more descriptive names under CP group
* add option to enable moving where there is no data
* add test for param CP_GO_NO_DATA
Co-Authored-By: Martina Rivizzigno <martina@rivizzigno.it>
Fixes a potential buffer overflow if an MC/helicopter mixer is used that
exceeds the number of physical pins.
This is not a useful/flyable configuration, but the system still should
not crash.
PX4 BuildBot