This change is necessary to give the pilot the ability to switch VTOL state
even if for some reason no attitude sp are published anymore.
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
-move pusher assist functionality into vtol_type class and adapt it to also
work for tiltrotor VTOLs (pitch rotors down to accelerate forward)
-for tiltrotor: compensate for lost lift due to tilt by increasing the throttle
-enable pusher / tiltassist also in altitude mode
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
* 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
* adds a work_queue systemcmd that will bring a tree view of all active work queues and work items
* WorkQueues now track attached WorkItems and will shutdown when the last WorkItem is detached
- VT_MOT_COUNT assumed that motors were always the first outputs. This
does not have to be true always. VT_MOT_ID allows to specify precisely how
many motors we have for hovering and to which channel they are connected.
Signed-off-by: RomanBapst <bapstroman@gmail.com>
This changes the enums used for various VTOL states to enum classes
which makes them type-safe and should avoid shadowing.
This change was motivated by a Clang warning about shadowing of the
enum const TRANSITION_TO_FW which was declared twice, once in
vtol_type.h and once in standard.h.
This change only removes the shadowing but presumably these enums could
be cleaned up and consolidated further.
* VTOL trans: changed that now in transition for both MC and FW the corresponding (correct) attitude controller is running
* attitude setpoint for stabilized mode is generated by tailsitter.cpp
* reset yaw setpoint during transition to avoid big yaw errors after
transition back to hover
* VT_TYPE parameter: added "reboot required" metadata
Mark V19_VT_ROLLDIR @category system
Throttle down mavlink critical msg
Send 0 actuator_output for safety
VTOL: unset v1.9 roll direction safety check param for builtin airframes
* attitude and rate setpoint message: use 3D array for thrust demand
* FixedWingAttitudeControl: rework airspeed scaling
* move airspeed and scaling calculation into separate method
* if vtol in hover and airspeed disabled use minimum airspeed instead of trim airspeed
- moved methods used to modify channel maximum pwm value to VtolType
class so that the can be shared by the differnt vtol types
Signed-off-by: Roman <bapstroman@gmail.com>
Since assertions lead to crashes, we need better failure handling. In all
the cases in this patch, the assert is not required.
All the ones with the task id should be replaced with the module base
class.
Ah yes, and this reduces flash space, since the ASSERT macro will expand to
a printf that contains the source file name.
- standard vtol was implementing many custom parameters although they
are generic and should be shared between the vtol types
- removed heavy usage of hrt_elapsed_time() which is a system call and
could be computationally expensive
Previously transition commands were not acked at all which meant that a
mavlink consumer such as a ground station would not get feedback if the
command arrived.
This solution is not optimal because it does not take into account if
the transition actually happened but at least it is feedback that the
command has arrived at the destination.
RomanBapst