* introduced altitude acceptance radius in position setpoint for fixed
wing guidance
- allows navigator to explicitly set the altitude acceptance radius
- needed for staright line landing support
* added ignore_alt_acceptance to position setpoint message to allow guidance
logic to ignore altitude error on waypoint
- can be useful to prevent loitering at a waypoint within a mission landing sequence
* only set altitude acceptance radius to infinity for a waypoint inside a mission landing
for fixed wing vehicles
* navigator: return altitude acceptance radius from triplet if it's valid
* FixedWingPositionControl: check if alt acceptance radius provided in position setpoint
is larger 0
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Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Alvaro Fernandez <alvaro@auterion.com>
This will send the System message if it is already being sent by a ground
station. Otherwise, it will assemble the message itself using the
takeoff/home location.
Improve the slow down effect and add support for speed change in mission mode.
Seperate code related to turning setpoints into motor commands into its own folder and refactor code.
This is similar to fake pos but is only used when the ekf has an
external information telling it that the vehicle is not changing
position. This information can then be used to keep a valid local
position even when the vehicle isn't exactly at rest.
* Remove euler angles from attitude setpoint message
* Remove usage of euler angles in attitude setpoint messages
This commit removes the usage of euler angles in the vehicle_attitude_setpoint messages
* Fix standard vtol
* added support for resetting wind states to external observation
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* moved wind related functions into separate file
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* added VEHICLE_CMD_EXTERNAL_WIND_ESTIMATE
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* correctly compute variances
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* ekf2: implement wind reset
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* only allow VEHICLE_CMD_EXTERNAL_WIND_ESTIMATE during wind dead-reckoning
and increase horizontal velocity variance to allow velocity states to move
towards solution that is aligned with the newly set wind
Signed-off-by: RomanBapst <bapstroman@gmail.com>
* only reset wind on ground
* still use wind reset using airspeed when it wasn't initialized
* exclude func for rover, change reset interface
* handle wind reset in drag-fusion
* replace state reset with variance reset in sideslip/drag fusion
* remove resetWind function
---------
Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Marco Hauswirth <marco.hauswirth@auterion.com>
- remove commander test ratio "tuning knobs" (COM_ARM_EKF_{HGT,POS,VEL,YAW})
- these are effectively redundant with the actual tuning (noise & gate)
in the estimator, plus most users have no idea why they'd be
adjusting these other than to silence an annoying preflight complaint
- remove ekf2 "PreFlightChecker" with hard coded innovation limits
- ekf2 preflight innovation flags are now simply if any active source
exceeds half the limit preflight
* estimator gps check fail flag for spoofing
* warn whenever spoofing state changes to true, use default hysteresis to completely stop fusion
* dont introduce more GPS namings, GNSS instead
* flash: exclude mantis for cuav_x7pro
