ControlAllocator: enable custom saturation logic to override default one

Custom saturation logic currently implemented for Tiltrotor VTOL and Helicopter.

Signed-off-by: Silvan Fuhrer <silvan@auterion.com>

src/modules/control_allocator/ActuatorEffectiveness/ActuatorEffectiveness.hpp

@@ -199,10 +199,10 @@ public:
 	virtual uint32_t getStoppedMotors() const { return 0; }
 
 	/**
-	 * Fill in the allocated and unallocated torque and thrust.
-	 * Should return false if not filled in and the effectivenes matrix should be used instead
+	 * Fill in the allocated and unallocated torque and thrust, customized by effectiveness type.
+	 * Can be implemented for every type separately. If not implemented then the effectivenes matrix is used instead.
 	 */
-	virtual bool getAllocatedAndUnallocatedControl(control_allocator_status_s &status) const { return false; }
+	virtual void getAllocatedAndUnallocatedControl(int matrix_index, control_allocator_status_s &status) {}
 
 protected:
 	FlightPhase _flight_phase{FlightPhase::HOVER_FLIGHT};		///< Current flight phase

src/modules/control_allocator/ActuatorEffectiveness/ActuatorEffectivenessHelicopter.cpp

@@ -217,48 +217,37 @@ void ActuatorEffectivenessHelicopter::setSaturationFlag(float coeff, bool &posit
 	}
 }
 
-bool ActuatorEffectivenessHelicopter::getAllocatedAndUnallocatedControl(control_allocator_status_s &status) const
+void ActuatorEffectivenessHelicopter::getAllocatedAndUnallocatedControl(int matrix_index,
+		control_allocator_status_s &status)
 {
-	status.torque_setpoint_achieved = true;
-	status.thrust_setpoint_achieved = true;
 
 	// Note: the values '-1', '1' and '0' are just to indicate a negative,
 	// positive or no saturation to the rate controller. The actual magnitude is not used.
 	if (_saturation_flags.roll_pos) {
 		status.unallocated_torque[0] = 1.f;
-		status.torque_setpoint_achieved = false;
 
 	} else if (_saturation_flags.roll_neg) {
 		status.unallocated_torque[0] = -1.f;
-		status.torque_setpoint_achieved = false;
 	}
 
 	if (_saturation_flags.pitch_pos) {
 		status.unallocated_torque[1] = 1.f;
-		status.torque_setpoint_achieved = false;
 
 	} else if (_saturation_flags.pitch_neg) {
 		status.unallocated_torque[1] = -1.f;
-		status.torque_setpoint_achieved = false;
 	}
 
 	if (_saturation_flags.yaw_pos) {
 		status.unallocated_torque[2] = 1.f;
-		status.torque_setpoint_achieved = false;
 
 	} else if (_saturation_flags.yaw_neg) {
 		status.unallocated_torque[2] = -1.f;
-		status.torque_setpoint_achieved = false;
 	}
 
 	if (_saturation_flags.thrust_pos) {
 		status.unallocated_thrust[2] = 1.f;
-		status.thrust_setpoint_achieved = false;
 
 	} else if (_saturation_flags.thrust_neg) {
 		status.unallocated_thrust[2] = -1.f;
-		status.thrust_setpoint_achieved = false;
 	}
-
-	return true;
 }

src/modules/control_allocator/ActuatorEffectiveness/ActuatorEffectivenessHelicopter.hpp

@@ -79,7 +79,7 @@ public:
 			    ActuatorVector &actuator_sp, const matrix::Vector<float, NUM_ACTUATORS> &actuator_min,
 			    const matrix::Vector<float, NUM_ACTUATORS> &actuator_max) override;
 
-	bool getAllocatedAndUnallocatedControl(control_allocator_status_s &status) const override;
+	void getAllocatedAndUnallocatedControl(int matrix_index, control_allocator_status_s &status) override;
 private:
 	float throttleSpoolupProgress();
 	bool mainMotorEnaged();

src/modules/control_allocator/ActuatorEffectiveness/ActuatorEffectivenessTiltrotorVTOL.cpp

@@ -147,6 +147,21 @@ void ActuatorEffectivenessTiltrotorVTOL::updateSetpoint(const matrix::Vector<flo
 			}
 		}
 	}
+
+	// Set yaw saturation flag in case of yaw through tilt. As in this case the yaw actuation is decoupled from
+	// the other axes (for now neglecting the case of 0 collective thrust), we set the saturation flags
+	// directly if the (normalized) yaw torque setpoint is outside of range (-1, 1).
+	if (matrix_index == 0 && _tilts.hasYawControl()) {
+		_yaw_tilt_saturation_flags.tilt_yaw_neg = false;
+		_yaw_tilt_saturation_flags.tilt_yaw_pos = false;
+
+		if (control_sp(2) < -1.f) {
+			_yaw_tilt_saturation_flags.tilt_yaw_neg = true;
+
+		} else if (control_sp(2) > 1.f) {
+			_yaw_tilt_saturation_flags.tilt_yaw_pos = true;
+		}
+	}
 }
 
 void ActuatorEffectivenessTiltrotorVTOL::setFlightPhase(const FlightPhase &flight_phase)
@@ -170,3 +185,24 @@ void ActuatorEffectivenessTiltrotorVTOL::setFlightPhase(const FlightPhase &fligh
 		break;
 	}
 }
+
+void ActuatorEffectivenessTiltrotorVTOL::getAllocatedAndUnallocatedControl(int matrix_index,
+		control_allocator_status_s &status)
+{
+	// only handle matrix 0 (motors and tilts)
+	if (matrix_index == 1) {
+		return;
+	}
+
+	// Note: the values '-1', '1' and '0' are just to indicate a negative,
+	// positive or no saturation to the rate controller. The actual magnitude is not used.
+	if (_yaw_tilt_saturation_flags.tilt_yaw_pos) {
+		status.unallocated_torque[2] = 1.f;
+
+	} else if (_yaw_tilt_saturation_flags.tilt_yaw_neg) {
+		status.unallocated_torque[2] = -1.f;
+
+	} else {
+		status.unallocated_torque[2] = 0.f;
+	}
+}

src/modules/control_allocator/ActuatorEffectiveness/ActuatorEffectivenessTiltrotorVTOL.hpp

@@ -81,6 +81,9 @@ public:
 	const char *name() const override { return "VTOL Tiltrotor"; }
 
 	uint32_t getStoppedMotors() const override { return _stopped_motors; }
+
+	void getAllocatedAndUnallocatedControl(int matrix_index, control_allocator_status_s &status) override;
+
 protected:
 	bool _collective_tilt_updated{true};
 	ActuatorEffectivenessRotors _mc_rotors;
@@ -97,4 +100,11 @@ protected:
 
 	uORB::Subscription _actuator_controls_1_sub{ORB_ID(actuator_controls_1)};
 	uORB::Subscription _actuator_controls_0_sub{ORB_ID(actuator_controls_0)};
+
+	struct YawTiltSaturationFlags {
+		bool tilt_yaw_pos;
+		bool tilt_yaw_neg;
+	};
+
+	YawTiltSaturationFlags _yaw_tilt_saturation_flags{};
 };