* FW attitude controller, FW position controller and VTOL attitude controller subscribe to airspeed_validated topic
* add possibility to switch off the airspeed valid checks
* remove airspeed valid checks from commander
* clean up of VTOL transition logic
* Airspeed Selector: remove dynamic allocation of airspeed validators (depending on number of connected sensors) but do it statically for the maximum number allowed. Check for number of connected sensors not only during start up, but always when vehicle is disarmed.
* Airspeed Selector: change work queue from lp to att_pos_ctrl as this module is safety-critical
* add airspeed selector to px4_fmu-v2 defaults
* PreFlightCheck: remove unused reportFailures flag
* Commander: pull all pre flight checks together on the PreFlightCheck class
* PreFlightCheck: separate checks into their own files
When flying POSCTL and ALTCTL the throttle stick is usually spring
loaded and therefore centered. Therefore, it makes more sense to check
for above center instead of above low.
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)
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".
added and using circuit_breaker_enabled_by_val() where possible instead of circuit_breaker_enabled() which search for cbrk parameters by name, which is extensive process.
Condition to enter the prearmed state, an intermediate state between disarmed and armed
* in which non-throttling actuators are active.
*
* @value 0 Disabled
* @value 1 Safety button
* @value 2 Always
* the large 20% margin is no longer appropriate now that nearly all work in the system is
scheduled (moved out of ISRs) and represented in the load percentage
* closes https://github.com/PX4/Firmware/issues/12753
This allows to bypass preflight and prearm checks.
During development there are regular cases where I just want to arm the
board/vehicle no matter what, and the preflight checks are guaranteed to
fail (e.g. sensors uncalibrated, inconsistent, powered via USB, etc.).
Allowing an easy and quick way to arm (assuming you know what you are
doing) helps to speed up development considerably and is less frustrating.
