2 changed files with 177 additions and 0 deletions
@ -0,0 +1,106 @@ |
|||||||
|
/****************************************************************************
|
||||||
|
* |
||||||
|
* 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 FlightManualStabilized.cpp |
||||||
|
* |
||||||
|
* Flight task for manual controlled attitude. |
||||||
|
* It generates thrust and yaw setpoints. |
||||||
|
* TODO: add thrust |
||||||
|
*/ |
||||||
|
|
||||||
|
#include "FlightTaskManualStabilized.hpp" |
||||||
|
#include <mathlib/mathlib.h> |
||||||
|
#include <float.h> |
||||||
|
#include <lib/geo/geo.h> |
||||||
|
|
||||||
|
using namespace matrix; |
||||||
|
|
||||||
|
FlightTaskManualStabilized::FlightTaskManualStabilized(control::SuperBlock *parent, const char *name) : |
||||||
|
FlightTaskManual(parent, name), |
||||||
|
_yaw_rate_scaling(parent, "MPC_MAN_Y_MAX", false) |
||||||
|
{} |
||||||
|
|
||||||
|
bool FlightTaskManualStabilized::activate() |
||||||
|
{ |
||||||
|
_yaw_sp = _yaw; |
||||||
|
_yaw_rate_sp = 0.0f; |
||||||
|
_sign_speed = 1.0f; |
||||||
|
return FlightTaskManual::activate(); |
||||||
|
} |
||||||
|
|
||||||
|
void FlightTaskManualStabilized::_scaleSticks() |
||||||
|
{ |
||||||
|
/* Scale sticks to yaw and thrust using
|
||||||
|
* linear scale. |
||||||
|
* TODO: add thrust */ |
||||||
|
_yaw_rate_sp = _sticks(3) * math::radians(_yaw_rate_scaling.get()); |
||||||
|
} |
||||||
|
|
||||||
|
void FlightTaskManualStabilized::_updateHeadingSetpoints() |
||||||
|
{ |
||||||
|
/* Yaw-lock depends on stick input. If locked,
|
||||||
|
* yawspeed_sp is set to NAN. Otherwise yaw_sp is set |
||||||
|
* to NAN.*/ |
||||||
|
const bool stick_yaw_zero = fabsf(_sticks(3)) <= _stick_dz.get(); |
||||||
|
|
||||||
|
if (stick_yaw_zero && !PX4_ISFINITE(_yaw_sp)) { |
||||||
|
_yaw_sp = _wrap_pi(_yaw + _sign_speed * _yaw_rate_scaling.get() * _deltatime); |
||||||
|
|
||||||
|
} else if (!stick_yaw_zero) { |
||||||
|
_yaw_sp = NAN; |
||||||
|
_sign_speed = math::sign(_yaw_rate_sp); |
||||||
|
} |
||||||
|
} |
||||||
|
|
||||||
|
void FlightTaskManualStabilized::_updateThrustSetpoints() |
||||||
|
{ |
||||||
|
// TODO
|
||||||
|
} |
||||||
|
|
||||||
|
void FlightTaskManualStabilized::_updateSetpoints() |
||||||
|
{ |
||||||
|
_updateHeadingSetpoints(); |
||||||
|
//_updateThrustSetpoints();
|
||||||
|
} |
||||||
|
|
||||||
|
bool FlightTaskManualStabilized::update() |
||||||
|
{ |
||||||
|
_scaleSticks(); // scales sticks linearly to yaw/yawspeed and thrust
|
||||||
|
_updateSetpoints(); // applies yaw and position lock if required
|
||||||
|
_setYawSetpoint(_yaw_sp); |
||||||
|
_setYawspeedSetpoint(_yaw_rate_sp); |
||||||
|
//_setThrustSetpoint(...) TODO
|
||||||
|
|
||||||
|
return true; |
||||||
|
} |
@ -0,0 +1,71 @@ |
|||||||
|
/****************************************************************************
|
||||||
|
* |
||||||
|
* 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 FlightManualStabilized.hpp |
||||||
|
* |
||||||
|
* Flight task for manual controlled attitude. |
||||||
|
* It generates thrust and yaw setpoints. |
||||||
|
* TODO: add thrust |
||||||
|
*/ |
||||||
|
|
||||||
|
#pragma once |
||||||
|
|
||||||
|
#include "FlightTaskManual.hpp" |
||||||
|
|
||||||
|
class FlightTaskManualStabilized : public FlightTaskManual |
||||||
|
{ |
||||||
|
public: |
||||||
|
FlightTaskManualStabilized(control::SuperBlock *parent, const char *name); |
||||||
|
|
||||||
|
virtual ~FlightTaskManualStabilized() = default; |
||||||
|
|
||||||
|
bool activate() override; |
||||||
|
|
||||||
|
bool update() override; |
||||||
|
|
||||||
|
protected: |
||||||
|
float _yaw_rate_sp{}; /**< Scaled yaw rate from stick. NAN if yaw is locked. */ |
||||||
|
float _yaw_sp{}; /**< Yaw setpoint once locked. Otherwise NAN. */ |
||||||
|
|
||||||
|
virtual void _updateSetpoints(); /**< Updates all setpoints. */ |
||||||
|
virtual void _scaleSticks(); /**< Scales sticks to yaw and thrust. */ |
||||||
|
|
||||||
|
private: |
||||||
|
float _sign_speed{}; |
||||||
|
void _updateHeadingSetpoints(); /**< Sets yaw or yaw speed. */ |
||||||
|
void _updateThrustSetpoints(); /**< Sets thrust setpoint */ |
||||||
|
|
||||||
|
control::BlockParamFloat _yaw_rate_scaling; /**< Scaling factor from stick to yaw rate. */ |
||||||
|
|
||||||
|
}; |
Loading…
Reference in new issue