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FlightTaskManual.cpp
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/****************************************************************************
*
* Copyright (c) 2018 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 FlightTaskManual.cpp
*/
#include "FlightTaskManual.hpp"
#include <mathlib/mathlib.h>
#include <float.h>
#include <drivers/drv_hrt.h>
using namespace matrix;
using namespace time_literals;
bool FlightTaskManual::updateInitialize()
{
bool ret = FlightTask::updateInitialize();
_sub_manual_control_setpoint.update();
const bool sticks_available = _evaluateSticks();
if (_sticks_data_required) {
ret = ret && sticks_available;
}
return ret;
}
bool FlightTaskManual::_evaluateSticks()
{
hrt_abstime rc_timeout = (_param_com_rc_loss_t.get() * 1.5f) * 1_s;
/* Sticks are rescaled linearly and exponentially to [-1,1] */
if ((_time_stamp_current - _sub_manual_control_setpoint.get().timestamp) < rc_timeout) {
/* Linear scale */
_sticks(0) = _sub_manual_control_setpoint.get().x; /* NED x, "pitch" [-1,1] */
_sticks(1) = _sub_manual_control_setpoint.get().y; /* NED y, "roll" [-1,1] */
_sticks(2) = -(_sub_manual_control_setpoint.get().z - 0.5f) * 2.f; /* NED z, "thrust" resacaled from [0,1] to [-1,1] */
_sticks(3) = _sub_manual_control_setpoint.get().r; /* "yaw" [-1,1] */
/* Exponential scale */
_sticks_expo(0) = math::expo_deadzone(_sticks(0), _param_mpc_xy_man_expo.get(), _param_mpc_hold_dz.get());
_sticks_expo(1) = math::expo_deadzone(_sticks(1), _param_mpc_xy_man_expo.get(), _param_mpc_hold_dz.get());
_sticks_expo(2) = math::expo_deadzone(_sticks(2), _param_mpc_z_man_expo.get(), _param_mpc_hold_dz.get());
_sticks_expo(3) = math::expo_deadzone(_sticks(3), _param_mpc_yaw_expo.get(), _param_mpc_hold_dz.get());
// Only switch the landing gear up if the user switched from gear down to gear up.
// If the user had the switch in the gear up position and took off ignore it
// until he toggles the switch to avoid retracting the gear immediately on takeoff.
int8_t gear_switch = _sub_manual_control_setpoint.get().gear_switch;
if (_gear_switch_old != gear_switch) {
_applyGearSwitch(gear_switch);
}
_gear_switch_old = gear_switch;
// valid stick inputs are required
const bool valid_sticks = PX4_ISFINITE(_sticks(0))
&& PX4_ISFINITE(_sticks(1))
&& PX4_ISFINITE(_sticks(2))
&& PX4_ISFINITE(_sticks(3));
return valid_sticks;
} else {
/* Timeout: set all sticks to zero */
_sticks.zero();
_sticks_expo.zero();
_gear.landing_gear = landing_gear_s::GEAR_KEEP;
return false;
}
}
void FlightTaskManual::_applyGearSwitch(uint8_t gswitch)
{
if (gswitch == manual_control_setpoint_s::SWITCH_POS_OFF) {
_gear.landing_gear = landing_gear_s::GEAR_DOWN;
}
if (gswitch == manual_control_setpoint_s::SWITCH_POS_ON) {
_gear.landing_gear = landing_gear_s::GEAR_UP;
}
}