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bizhang_-obav/src/lib/FlightTasks/tasks/FlightTaskManualAltitude.cpp

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/****************************************************************************
*
* Copyright (c) 2017 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file FlightManualAltitude.cpp
*/
#include "FlightTaskManualAltitude.hpp"
#include <float.h>
using namespace matrix;
void FlightTaskManualAltitude::_scaleSticks()
{
/* Reuse same scaling as for stabilized */
FlightTaskManualStabilized::_scaleSticks();
/* Scale horizontal velocity with expo curve stick input*/
const float vel_max_z = (_sticks(2) > 0.0f) ? _limits.speed_dn_max : _limits.speed_up_max;
_velocity_setpoint(2) = vel_max_z * _sticks_expo(2);
}
void FlightTaskManualAltitude::_updateAltitudeLock()
{
/* Depending on stick inputs and velocity, position is locked.
* If not locked, altitude setpoint is set to NAN.
*/
/* handle position and altitude hold */
const bool apply_brake_z = fabsf(_velocity_setpoint(2)) <= FLT_EPSILON;
const bool stopped_z = (MPC_HOLD_MAX_Z.get() < FLT_EPSILON || fabsf(_velocity(2)) < MPC_HOLD_MAX_Z.get());
if (apply_brake_z && stopped_z && !PX4_ISFINITE(_position_setpoint(2))) {
_position_setpoint(2) = _position(2);
} else if (!apply_brake_z) {
_position_setpoint(2) = NAN;
}
}
void FlightTaskManualAltitude::_updateSetpoints()
{
FlightTaskManualStabilized::_updateSetpoints(); // get yaw and thrust setpoints
_thrust_setpoint *= NAN; // Don't need thrust setpoint from Stabilized mode.
/* Thrust in xy are extracted directly from stick inputs. A magnitude of
* 1 means that maximum thrust along xy is required. A magnitude of 0 means no
* thrust along xy is required. The maximum thrust along xy depends on the thrust
* setpoint along z-direction, which is computed in PositionControl.cpp.
*/
Vector2f sp{_sticks(0), _sticks(1)};
_rotateIntoHeadingFrame(sp);
if (sp.length() > 1.0f) {
sp.normalize();
}
_thrust_setpoint(0) = sp(0);
_thrust_setpoint(1) = sp(1);
_updateAltitudeLock();
}