- in practice this is mostly useful for identifying incorrect rotations
which we mostly have in 45 degree increments
- handling a vehicle on the ground can easily disturb one mag by more than 30 degrees, so this is often distracting noise
- if "landed" and "maybe_landed" states are false then both the "hit_ground" and the "low_thrust" condition need to be true in order to detect landing
- ground contact MC NAN setpoint workaround
- ground contact additionally check acceleration setpoint
- schedule with vehicle_local_position updates (most updates require valid local position)
- don't allow LNDMC_Z_VEL_MAX to exceed MPC_LAND_SPEED
- ground contact horizontal movement checks default to failed if estimates aren't available
This fixes the takeoff and land CI test where we do a takeoff and land
without RC connected.
In my opinion it does not make sense to go into RC lost failsafe if
a datalink is still available.
Of course, this can be dangerous if someone has a companion computer
connected which gets detected as "data link" but actually has no
connection to the ground station.
This removes the check for the current position of the VTOL swtich, as arming is already prevented if in transition mode,
plus also if VTOL and in fixed-wing mode (unless CBRK_VTOL_ARMING is set).
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
- Introduced COM_LKDOWN_TKO parameter
- Introduced auto disarm for lockdown state
- Do not trigger flight termiantion if system is in lockdown
Signed-off-by: Claudio Micheli <claudio@auterion.com>
- remove all remaining IOCTLs for accel and gyro and handle all calibration entirely in sensors module with parameters
- sensor_accel and sensor_gyro are now always raw sensor data
- calibration procedures no longer need to first clear existing values before starting
- temperature calibration (TC) remove all scale (SCL) parameters
- gyro and baro scale are completely unused
- regular accel calibration scale can be used (CAL_ACC*_xSCALE) instead of TC scale
A parameter spcifies what the redundancy level for 5V rail supply
needs to be and a check makes sure that it's available before
taking off such that the user is aware of a broken or disconnected
redundant power module.
Because of warnings on every flight on setups without
any need for concern. Some even high quality supply voltage regulators
that are rated for 5V can with tolerances and load get lower than 4.9V.
- skip avionics rail voltage check when USB connected
- skip forced reboot on USB disconnect if circuit breaker set
- avionics voltage preflight check don't silently fail if system_power unavailble
- explicitly set supply check circuit breaker (CBRK_SUPPLY_CHK)
- always check with state machine before reboot/shutdown
- respect BOARD_HAS_POWER_CONTROL (shutdown from command, low battery, power button)
- px4_shutdown_request add optional delay and always execute from HPWORK
- px4_shutdown_request split out px4_reboot_request
- create common uORB::PublicationBase
- uORB::PublicationQueued types are now type aliases
- ORB_PRIO use enum type everywhere to avoid accidental misuse
- PX4Accelerometer/PX4Gyroscope/etc driver libs explicitly advertise on construction, unadvertise on destruction. This is a workaround for any potential issues that might appear when accel/gyro cdev and uORB indexing doesn't align.
* commander: add check for VTOL airfame on fmu-v2
This adds a preflight check when a VTOL airframe is configured
on a fmu-v2 where VTOL is no longer included.
* commander: address code review comments
Daniel Agar