Files
PX4-Autopilot/src/modules/control_allocator/ActuatorEffectiveness/ActuatorEffectivenessStandardVTOL.hpp
T
Silvan Fuhrer 1e56d9c219 Rework flaps/spoilers logic
- remove deprecated actuator_controls[INDEX_FLAPS/SPOILERS/AIRBRAKES]
- use new topic normalized_unsigned_setpoint.msg (with instances flaps_setpoint
and spoilers_setpoint) to pass into control allocation
- remove flaps/spoiler related fields from attitude_setpoint topic
- CA: add possibility to map flaps/spoilers to any control surface
- move flaps/spoiler pitch trimming to CA (previously called DTRIM_FLAPS/SPOILER)
- move manual flaps/spoiler handling from rate to attitude controller

FW Position controller: change how negative switch readings are intepreted
for flaps/spoilers (considered negative as 0).

VTOL: Rework spoiler publishing in hover

- pushlish spoiler_setpoint.msg in the VTOL module if in hover
- also set spoilers to land configuration if in Descend mode

Allocation: add slew rate limit of 0.5 to flaps/spoilers configuration change

Instead of doing the flaps/spoilers slew rate limiting in the FW Position Controller
(which then only is applied in Auto flight), do it consistently over all flight
modes, so also for manual modes.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
2023-03-06 22:43:41 +01:00

95 lines
3.6 KiB
C++

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/**
* @file ActuatorEffectivenessStandardVTOL.hpp
*
* Actuator effectiveness for standard VTOL
*
* @author Julien Lecoeur <julien.lecoeur@gmail.com>
*/
#pragma once
#include "ActuatorEffectiveness.hpp"
#include "ActuatorEffectivenessRotors.hpp"
#include "ActuatorEffectivenessControlSurfaces.hpp"
#include <uORB/topics/normalized_unsigned_setpoint.h>
class ActuatorEffectivenessStandardVTOL : public ModuleParams, public ActuatorEffectiveness
{
public:
ActuatorEffectivenessStandardVTOL(ModuleParams *parent);
virtual ~ActuatorEffectivenessStandardVTOL() = default;
bool getEffectivenessMatrix(Configuration &configuration, EffectivenessUpdateReason external_update) override;
const char *name() const override { return "Standard VTOL"; }
int numMatrices() const override { return 2; }
void getDesiredAllocationMethod(AllocationMethod allocation_method_out[MAX_NUM_MATRICES]) const override
{
static_assert(MAX_NUM_MATRICES >= 2, "expecting at least 2 matrices");
allocation_method_out[0] = AllocationMethod::SEQUENTIAL_DESATURATION;
allocation_method_out[1] = AllocationMethod::PSEUDO_INVERSE;
}
void getNormalizeRPY(bool normalize[MAX_NUM_MATRICES]) const override
{
normalize[0] = true;
normalize[1] = false;
}
void allocateAuxilaryControls(const float dt, int matrix_index, ActuatorVector &actuator_sp) override;
void setFlightPhase(const FlightPhase &flight_phase) override;
uint32_t getStoppedMotors() const override { return _stopped_motors; }
private:
ActuatorEffectivenessRotors _rotors;
ActuatorEffectivenessControlSurfaces _control_surfaces;
uint32_t _mc_motors_mask{}; ///< mc motors (stopped during forward flight)
uint32_t _stopped_motors{}; ///< currently stopped motors
int _first_control_surface_idx{0}; ///< applies to matrix 1
uORB::Subscription _flaps_setpoint_sub{ORB_ID(flaps_setpoint)};
uORB::Subscription _spoilers_setpoint_sub{ORB_ID(spoilers_setpoint)};
};