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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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FlightTaskManualPosition: remove update method and old member variable setpoints
This commit is contained in:
committed by
Beat Küng
parent
a7f4859698
commit
d6fe2159ae
@@ -1,6 +1,6 @@
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/****************************************************************************
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/****************************************************************************
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*
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*
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* Copyright (c) 2017 PX4 Development Team. All rights reserved.
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* Copyright (c) 2018 PX4 Development Team. All rights reserved.
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*
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*
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* Redistribution and use in source and binary forms, with or without
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* modification, are permitted provided that the following conditions
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@@ -50,15 +50,14 @@ FlightTaskManualPosition::FlightTaskManualPosition(control::SuperBlock *parent,
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bool FlightTaskManualPosition::activate()
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bool FlightTaskManualPosition::activate()
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{
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{
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_pos_sp_xy = matrix::Vector2f(NAN, NAN);
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bool ret = FlightTaskManualAltitude::activate();
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_vel_sp_xy = matrix::Vector2f(0.0f, 0.0f);
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_vel_sp(0) = _vel_sp(1) = 0.0f;
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return FlightTaskManualAltitude::activate();
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return ret;
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}
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}
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void FlightTaskManualPosition::_scaleSticks()
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void FlightTaskManualPosition::_scaleSticks()
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{
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{
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/* Use same scaling as for FlightTaskManualAltitude to
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/* Use same scaling as for FlightTaskManualAltitude */
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* get yaw and z */
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FlightTaskManualAltitude::_scaleSticks();
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FlightTaskManualAltitude::_scaleSticks();
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/* Constrain length of stick inputs to 1 for xy*/
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/* Constrain length of stick inputs to 1 for xy*/
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@@ -71,47 +70,36 @@ void FlightTaskManualPosition::_scaleSticks()
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}
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}
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/* Scale to velocity.*/
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/* Scale to velocity.*/
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_vel_sp_xy = stick_xy * _vel_xy_manual_max.get();
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matrix::Vector2f vel_sp_xy = stick_xy * _vel_xy_manual_max.get();
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/* Rotate setpoint into local frame. */
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/* Rotate setpoint into local frame. */
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matrix::Quatf q_yaw = matrix::AxisAnglef(matrix::Vector3f(0.0f, 0.0f, 1.0f), _yaw);
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matrix::Quatf q_yaw = matrix::AxisAnglef(matrix::Vector3f(0.0f, 0.0f, 1.0f), _yaw);
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matrix::Vector3f vel_world = q_yaw.conjugate(matrix::Vector3f(_vel_sp_xy(0), _vel_sp_xy(1), 0.0f));
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matrix::Vector3f vel_world = q_yaw.conjugate(matrix::Vector3f(vel_sp_xy(0), vel_sp_xy(1), 0.0f));
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_vel_sp_xy = matrix::Vector2f(vel_world(0), vel_world(1));
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_vel_sp(0) = vel_world(0);
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_vel_sp(1) = vel_world(1);
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}
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}
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void FlightTaskManualPosition::_updateXYlock()
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void FlightTaskManualPosition::_updateXYlock()
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{
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{
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/* If position lock is not active, position setpoint is set to NAN.*/
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/* If position lock is not active, position setpoint is set to NAN.*/
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const float vel_xy_norm = Vector2f(&_velocity(0)).length();
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const float vel_xy_norm = Vector2f(&_velocity(0)).length();
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const bool apply_brake = _vel_sp_xy.length() < FLT_EPSILON;
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const bool apply_brake = Vector2f(&_vel_sp(0)).length() < FLT_EPSILON;
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const bool stopped = (_vel_hold_thr_xy.get() < FLT_EPSILON || vel_xy_norm < _vel_hold_thr_xy.get());
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const bool stopped = (_vel_hold_thr_xy.get() < FLT_EPSILON || vel_xy_norm < _vel_hold_thr_xy.get());
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if (apply_brake && stopped && !PX4_ISFINITE(_pos_sp_xy(0))) {
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if (apply_brake && stopped && !PX4_ISFINITE(_pos_sp(0))) {
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_pos_sp_xy = matrix::Vector2f(&_position(0));
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_pos_sp(0) = _position(0);
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_pos_sp(1) = _position(1);
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} else if (!apply_brake) {
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} else if (!apply_brake) {
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/* Don't use position setpoint */
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/* don't lock*/
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_pos_sp_xy = _pos_sp_xy * NAN;
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_pos_sp(0) = NAN;
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_pos_sp(1) = NAN;
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}
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}
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}
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}
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void FlightTaskManualPosition::_updateSetpoints()
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void FlightTaskManualPosition::_updateSetpoints()
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{
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{
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FlightTaskManualAltitude::_updateSetpoints(); // get yaw and z setpoints
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FlightTaskManualAltitude::_updateSetpoints(); // needed to get yaw and setpoints in z-direction
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_thr_sp *= NAN; // don't require any thrust setpoints
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_updateXYlock(); // check for position lock
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_updateXYlock(); // check for position lock
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}
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}
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bool FlightTaskManualPosition::update()
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{
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_scaleSticks();
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_updateSetpoints();
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_setPositionSetpoint(Vector3f(_pos_sp_xy(0), _pos_sp_xy(1), _pos_sp_z));
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_setVelocitySetpoint(Vector3f(_vel_sp_xy(0), _vel_sp_xy(1), _vel_sp_z));
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_setYawSetpoint(_yaw_sp);
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_setYawspeedSetpoint(_yaw_rate_sp);
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_setThrustSetpoint(Vector3f(NAN, NAN, NAN));
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return true;
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}
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@@ -51,17 +51,12 @@ public:
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bool activate() override;
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bool activate() override;
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bool update() override;
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protected:
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protected:
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matrix::Vector2f _vel_sp_xy{}; /**< Scaled velocity setpoint from stick. NAN during position lock */
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control::BlockParamFloat _vel_xy_manual_max; /**< maximum speed allowed horizontally */
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matrix::Vector2f _pos_sp_xy{}; /**< Position setpoint during lock. Otherwise NAN */
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control::BlockParamFloat _acc_xy_max;/**< maximum acceleration horizontally. Only used to compute lock time */
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control::BlockParamFloat _vel_xy_manual_max; /**< Maximum speed allowed horizontally */
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control::BlockParamFloat _acc_xy_max;/**< Maximum acceleration horizontally. Only used to compute lock time */
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control::BlockParamFloat _vel_hold_thr_xy; /**< velocity threshold to switch back into horizontal position hold */
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control::BlockParamFloat _vel_hold_thr_xy; /**< velocity threshold to switch back into horizontal position hold */
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void _updateXYlock(); /**< Applies positon lock based on stick and velocity */
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void _updateXYlock(); /**< applies positon lock based on stick and velocity */
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void _updateSetpoints() override;
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void _updateSetpoints() override;
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void _scaleSticks() override;
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void _scaleSticks() override;
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};
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};
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