Internal combustion engine control module.
New actuator functions and RPM based start/restart logic.
Not enabled by default.
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Co-authored-by: Pernilla <pernilla@auterion.com>
* fix sign error in appropriate place
In PR https://github.com/PX4/PX4-Autopilot/pull/24175 I changed the
control surface deflection signs in generate_fw_aerodynamics to make the
1103 airframe work correctly. However, this breaks the 1101 airframe,
introducing sing errors there.
So, here the change in generate_fw_aerodynamics is reverted to the state
before PR #24175. Instead, the signs are set correctly by using
the HIL_ACT_REV bitfield in the respective airframe config files.
* match control surface parameters to SIH model
We want to align the default over all vehicle types for
this param. There are still some thresholds that are
increased for FW.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- we want the drivers, sensors hub, and estimator running as soon as possible to initialize and avoid commander false positives complaining about missing data
* add standard vtol airframe to SIH.
mostly took changes from 4d930bde and applied to main.
generate_fw_aerodynamics now takes four arguments rather than using the
_u class member, because depending on vehicle type _u is used
differently.
A user configurable delay for the internal `vehicle_local_position` seems confusing in my eyes. It's a different timeout for fixed-wing and multirotor which might have made sense earlier but not really anymore since the topic is constantly published by the estimator and not expected to time out on either vehicle type and the parameter description is also misleading because it's outdated.
The default implementation for multicopter Position mode is FlightTaskManualAcceleration.
The last missing piece was support for CollisionPrevention in this implementation.
* Added AUAV absolute pressure sensing
* Moved func to abstract base class
* Probe and params
* Fixed arg parsing and added auto start
* refactorings
* Added sample perf
* Fixed CI findings
* Simplified rc.sensors condition
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.
* 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
* lib: add FilteredDerivative class
* AirspeedValidator: add first principle check
- filters throttle, pitch and airspeed rate, and triggers
if the airspeed rate is negative even though the vehicle
is pitching down and giving high throttle.
Check has to fail for duration defined by ASPD_FP_T_WINDOW
to trigger an airspeed failure.
* AirspeedValidator: define constants for first principle check
* FilteredDerivative: set initialised to false if sample interval is invalid
* airspeed_selector: improved comment
* increase IAS derivative filter time constant from 4 to 5
* use legacy parameter handling for FW_PSP_OFF
* handle FW_THR_MAX as well
* ROMFS/airframes: exclude some airframes for v6x and v4pro to save flash on them
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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Silvan Fuhrer <silvan@auterion.com>
* reset position by fusion
* handle local_pos_valid for fixed wing in gnss denied
* [WIP] ekf2: setEkfGlobalOrigin respect current height reference and vertical position aiding
* global origin, also reset vertical pos without gps as ref
* fix wo gnss, that bitcraze ci passes
* revert some changes as requested
* remove duplicate reset messages
* undo unrelated whitespace changes, I'll fix it everywhere in a followup
* [SQUASH] ekf2: add vehicle_command_ack
* resetGlobalPosToExternalObservation consolidate logic
* remove gnss check from local_pos validation check
* reset when 0<accuracy<1, otherwise fuse
* replace gps param with flag
* ekf2: dead reckon time exceeded, respect ZUPT preflight if air data or optical flow expected
* subtract timeout from last inertial dead-reck, change fake pos conditions, save flash
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Co-authored-by: Daniel Agar <daniel@agar.ca>
The case where the airframe maintainer wants to enforce a reset to airframe is
not covered anymore with the `param set-default` mechanism. For products based
on PX4 this is still required to ensure proper functionality after a major update.
chfriedrich98