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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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navigator: wrote unit tests for Takeoff navigation mode
Signed-off-by: RomanBapst <bapstroman@gmail.com>
This commit is contained in:
parent
ad0482155e
commit
18a5bb32bc
@ -51,6 +51,7 @@ px4_add_module(
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enginefailure.cpp
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gpsfailure.cpp
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follow_target.cpp
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NavigatorCore.cpp
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DEPENDS
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git_ecl
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ecl_geo
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@ -59,4 +60,5 @@ px4_add_module(
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motion_planning
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)
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px4_add_functional_gtest(SRC RangeRTLTest.cpp LINKLIBS modules__navigator modules__dataman)
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px4_add_functional_gtest(SRC RangeRTLTest.cpp LINKLIBS modules__navigator modules__dataman)
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px4_add_functional_gtest(SRC NavigatorModeTakeoffTest.cpp LINKLIBS modules__navigator modules__dataman)
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17
src/modules/navigator/FakeNavigator.h
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17
src/modules/navigator/FakeNavigator.h
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@ -0,0 +1,17 @@
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#pragma once
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#define MODULE_NAME "navigator"
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#include <navigator/navigator.h>
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class FakeNavigator : public Navigator
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{
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public:
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FakeNavigator() :
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Navigator() {};
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virtual ~FakeNavigator() {};
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private:
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};
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@ -34,7 +34,7 @@
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#include <gtest/gtest.h>
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#include "geofence_breach_avoidance.h"
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#include "fake_geofence.hpp"
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#include "dataman_mocks.hpp"
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#include <dataman/dataman_mocks.hpp>
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#include <parameters/param.h>
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using namespace matrix;
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131
src/modules/navigator/NavigatorCore.cpp
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131
src/modules/navigator/NavigatorCore.cpp
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@ -0,0 +1,131 @@
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/***************************************************************************
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*
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* Copyright (c) 2021 PX4 Development Team. All rights reserved.
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*
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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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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file NavigatorCore.cpp
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*
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*/
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#include "NavigatorCore.h"
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#include <px4_platform_common/defines.h>
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NavigatorCore::NavigatorCore() :
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ModuleParams(nullptr)
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{
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}
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NavigatorCore::~NavigatorCore()
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{
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}
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bool NavigatorCore::forceVTOL()
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{
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return _status.is_vtol && (isRotaryWing() || _status.in_transition_to_fw) && _param_nav_force_vt.get();
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}
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float NavigatorCore::getHorAcceptanceRadiusMeter()
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{
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if (isRotaryWing()) {
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return getDefaultHorAcceptanceRadiusMeter();
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} else {
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return math::max(_pos_ctrl_status.acceptance_radius, getDefaultHorAcceptanceRadiusMeter());
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}
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}
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float NavigatorCore::getAltAcceptanceRadMeter()
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{
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if (isFixedWing()) {
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const position_setpoint_s &next_sp = getCurrentTriplet().next;
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if (next_sp.type == position_setpoint_s::SETPOINT_TYPE_LAND && next_sp.valid) {
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// Use separate (tighter) altitude acceptance for clean altitude starting point before landing
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return getFixedWingLandingAltAcceptanceRadius();
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}
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}
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return getDefaultAltAcceptanceRadiusMeter();
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}
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float NavigatorCore::getDefaultAltAcceptanceRadiusMeter()
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{
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if (isFixedWing()) {
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return getFixedWingAltAcceptanceRadiusMeter();
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} else if (isRover()) {
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return INFINITY;
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} else {
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float alt_acceptance_radius = getMulticopterAltAcceptanceRadiusMeter();
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if ((_pos_ctrl_status.timestamp > getCurrentTriplet().timestamp)
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&& _pos_ctrl_status.altitude_acceptance > alt_acceptance_radius) {
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alt_acceptance_radius = _pos_ctrl_status.altitude_acceptance;
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}
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return alt_acceptance_radius;
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}
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}
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float NavigatorCore::getAcceptanceRadiusMeter()
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{
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float acceptance_radius = _param_nav_acc_rad.get();
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// for fixed-wing and rover, return the max of NAV_ACC_RAD and the controller acceptance radius (e.g. L1 distance)
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if (!isRotaryWing() && PX4_ISFINITE(_pos_ctrl_status.acceptance_radius) && _pos_ctrl_status.timestamp != 0) {
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acceptance_radius = math::max(acceptance_radius, _pos_ctrl_status.acceptance_radius);
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}
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return acceptance_radius;
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}
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float NavigatorCore::getAltAcceptanceRadiusMeter()
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{
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if (isFixedWing()) {
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const position_setpoint_s &next_sp = _triplet.next;
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if (next_sp.type == position_setpoint_s::SETPOINT_TYPE_LAND && next_sp.valid) {
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// Use separate (tighter) altitude acceptance for clean altitude starting point before landing
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return _param_nav_fw_altl_rad.get();
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}
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}
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return getDefaultAltAcceptanceRadiusMeter();
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}
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157
src/modules/navigator/NavigatorCore.h
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157
src/modules/navigator/NavigatorCore.h
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@ -0,0 +1,157 @@
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/***************************************************************************
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*
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* Copyright (c) 2013-2017 PX4 Development Team. All rights reserved.
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*
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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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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
|
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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*/
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#include <px4_platform_common/module_params.h>
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#include <lib/mathlib/mathlib.h>
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#include <uORB/topics/vehicle_local_position.h>
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#include <uORB/topics/vehicle_status.h>
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#include <uORB/topics/vehicle_global_position.h>
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#include <uORB/topics/vehicle_land_detected.h>
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#include <uORB/topics/home_position.h>
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#include <uORB/topics/position_controller_status.h>
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#include <uORB/topics/position_setpoint_triplet.h>
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class NavigatorCore : public ModuleParams
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{
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public:
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NavigatorCore();
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~NavigatorCore();
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typedef matrix::Vector3<float> Vector3f;
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typedef matrix::Vector2<double> Vector2d;
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bool getLanded() { return _landed_state.landed; }
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bool getMaybeLanded() { return _landed_state.maybe_landed; }
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float getLandDetectedAltMaxMeter() { return _landed_state.alt_max; }
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double getLatRad() { return _global_pos.lat; }
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double getLonRad() { return _global_pos.lon;}
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float getAltitudeAMSLMeters() { return _global_pos.alt; }
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float getTrueHeadingRad() { return _local_pos.heading; }
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double getHomeLatRad() { return _home.lat; }
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double getHomeLonRad() { return _home.lon; }
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float getHomeAltAMSLMeter() { return _home.alt; }
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float getHomeTrueHeadingRad() { return _home.yaw; }
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home_position_s &getHomePosition() { return _home; }
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bool isNotArmed() { return _status.arming_state != vehicle_status_s::ARMING_STATE_ARMED; }
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uint8_t getArmingState() { return _status.arming_state; }
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float getPosNorthMeter() { return _local_pos.x; }
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float getPosEastMeter() { return _local_pos.y; }
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float getPosDownMeter() { return _local_pos.z; }
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float getVelNorthMPS() { return _local_pos.vx; }
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float getVelEastMPS() { return _local_pos.vy; }
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float getVelDownMPS() { return _local_pos.vz; }
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float getLoiterRadiusMeter() { return _param_nav_loiter_rad.get(); }
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bool getIsInTransitionMode() { return _status.in_transition_mode; }
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position_setpoint_triplet_s getCurrentTriplet() { return _triplet; }
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bool isHomeValid() { return (_home.timestamp > 0 && _home.valid_alt && _home.valid_hpos && _home.valid_lpos); }
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bool isHomeAltValid() { return (_home.timestamp > 0 && _home.valid_alt); }
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bool isRotaryWing() { return _status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING; }
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bool isFixedWing() { return _status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING; }
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bool isRover() { return _status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROVER; }
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bool isVTOL() { return _status.is_vtol; }
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uint8_t getVehicleType() { return _status.vehicle_type; }
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float getDefaultAltAcceptanceRadiusMeter();
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float getAltAcceptanceRadMeter();
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float getFixedWingLandingAltAcceptanceRadius() { return _param_nav_fw_altl_rad.get(); }
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float getDefaultHorAcceptanceRadiusMeter() { return _param_nav_acc_rad.get(); }
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float getHorAcceptanceRadiusMeter();
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float getMulticopterAltAcceptanceRadiusMeter() { return _param_nav_mc_alt_rad.get(); }
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float getFixedWingAltAcceptanceRadiusMeter() { return _param_nav_fw_alt_rad.get(); }
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float getAcceptanceRadiusMeter();
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float getAltAcceptanceRadiusMeter();
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float getRelativeTakeoffMinAltitudeMeter() { return _param_mis_takeoff_alt.get(); }
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float getRelativeLoiterMinAltitudeMeter() { return _param_mis_ltrmin_alt.get(); }
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bool isTakeoffRequired() { return _param_mis_takeoff_req.get(); }
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float getWaypointHeadingTimeoutSeconds() { return _param_mis_yaw_tmt.get(); }
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float getWaypointHeadingAcceptanceRad() { return _param_mis_yaw_err.get(); }
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bool forceVTOL();
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void updateLocalPosition(const vehicle_local_position_s &local_pos) { _local_pos = local_pos; };
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void updateVehicleStatus(const vehicle_status_s &status) { _status = status; }
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void updateGlobalPosition(const vehicle_global_position_s &global_pos) { _global_pos = global_pos; }
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void updateLandedState(const vehicle_land_detected_s &landed_state) { _landed_state = landed_state; }
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void updateHomePosition(const home_position_s &home) { _home = home; }
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void updatePositionControllerStatus(const position_controller_status_s &pos_ctrl_status) { _pos_ctrl_status = pos_ctrl_status; }
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private:
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vehicle_local_position_s _local_pos{};
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vehicle_status_s _status{};
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vehicle_global_position_s _global_pos{};
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vehicle_land_detected_s _landed_state{};
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home_position_s _home{};
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position_controller_status_s _pos_ctrl_status{};
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position_setpoint_triplet_s _triplet{};
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DEFINE_PARAMETERS(
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(ParamFloat<px4::params::NAV_LOITER_RAD>) _param_nav_loiter_rad, /**< loiter radius for fixedwing */
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(ParamFloat<px4::params::NAV_ACC_RAD>) _param_nav_acc_rad, /**< acceptance for takeoff */
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(ParamFloat<px4::params::NAV_FW_ALT_RAD>)
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_param_nav_fw_alt_rad, /**< acceptance radius for fixedwing altitude */
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(ParamFloat<px4::params::NAV_FW_ALTL_RAD>)
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_param_nav_fw_altl_rad, /**< acceptance radius for fixedwing altitude before landing*/
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(ParamFloat<px4::params::NAV_MC_ALT_RAD>)
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_param_nav_mc_alt_rad, /**< acceptance radius for multicopter altitude */
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(ParamInt<px4::params::NAV_FORCE_VT>) _param_nav_force_vt, /**< acceptance radius for multicopter altitude */
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(ParamInt<px4::params::NAV_TRAFF_AVOID>) _param_nav_traff_avoid, /**< avoiding other aircraft is enabled */
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(ParamFloat<px4::params::NAV_TRAFF_A_RADU>) _param_nav_traff_a_radu, /**< avoidance Distance Unmanned*/
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(ParamFloat<px4::params::NAV_TRAFF_A_RADM>) _param_nav_traff_a_radm, /**< avoidance Distance Manned*/
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// non-navigator parameters
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// Mission (MIS_*)
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(ParamFloat<px4::params::MIS_LTRMIN_ALT>) _param_mis_ltrmin_alt,
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(ParamFloat<px4::params::MIS_TAKEOFF_ALT>) _param_mis_takeoff_alt,
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(ParamBool<px4::params::MIS_TAKEOFF_REQ>) _param_mis_takeoff_req,
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(ParamFloat<px4::params::MIS_YAW_TMT>) _param_mis_yaw_tmt,
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(ParamFloat<px4::params::MIS_YAW_ERR>) _param_mis_yaw_err
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)
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};
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121
src/modules/navigator/NavigatorModeTakeoffTest.cpp
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121
src/modules/navigator/NavigatorModeTakeoffTest.cpp
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@ -0,0 +1,121 @@
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/****************************************************************************
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*
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* Copyright (C) 2021 PX4 Development Team. All rights reserved.
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*
|
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* 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.
|
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*
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****************************************************************************/
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#include <gtest/gtest.h>
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#include "FakeNavigator.h"
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#include "takeoff.h"
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#include <dataman/dataman_mocks.hpp>
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TEST(NavigatorModeTakeoffTest, TestTakeoff)
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{
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FakeNavigator fake_navigator;
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NavigatorCore &navigator_core = fake_navigator.getCore();
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Takeoff takeoff(&fake_navigator, navigator_core);
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fake_navigator.params_update();
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vehicle_status_s status = {};
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status.timestamp = 1e6;
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status.is_vtol = true;
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status.arming_state = vehicle_status_s::ARMING_STATE_ARMED;
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status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
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vehicle_global_position_s global_pos = {};
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global_pos.timestamp = 1e6;
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global_pos.lat = 40;
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global_pos.lon = 3;
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global_pos.alt = 300;
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vehicle_land_detected_s landed = {};
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landed.landed = true;
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landed.timestamp = 1e6;
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home_position_s home = {};
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home.timestamp = 1e6;
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home.lat = global_pos.lat;
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home.lon = global_pos.lon;
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home.alt = global_pos.alt;
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home.valid_alt = true;
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home.valid_hpos = true;
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home.valid_lpos = true;
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vehicle_local_position_s local_pos = {};
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local_pos.timestamp = 1e6;
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local_pos.x = -0.2f;
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local_pos.y = 0.1f;
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local_pos.z = 0.1f;
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local_pos.vx = local_pos.vy = local_pos.vz = 0;
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local_pos.heading = -0.54f;
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navigator_core.updateGlobalPosition(global_pos);
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navigator_core.updateHomePosition(home);
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navigator_core.updateLandedState(landed);
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navigator_core.updateLocalPosition(local_pos);
|
||||
navigator_core.updateVehicleStatus(status);
|
||||
|
||||
takeoff.on_activation();
|
||||
|
||||
position_setpoint_s current = fake_navigator.get_position_setpoint_triplet()->current;
|
||||
|
||||
ASSERT_EQ(current.lat, navigator_core.getLatRad());
|
||||
ASSERT_EQ(current.lon, navigator_core.getLonRad());
|
||||
ASSERT_EQ(current.type, 3); // position_setpoint_s::TYPE_TAKEOFF
|
||||
ASSERT_EQ(current.valid, true);
|
||||
ASSERT_EQ(current.alt_valid, true);
|
||||
ASSERT_EQ(current.alt, global_pos.alt + navigator_core.getRelativeTakeoffMinAltitudeMeter());
|
||||
ASSERT_EQ(current.yaw, navigator_core.getTrueHeadingRad());
|
||||
ASSERT_EQ(current.yaw_valid, true);
|
||||
ASSERT_EQ(current.yawspeed_valid, false);
|
||||
ASSERT_EQ(current.loiter_radius, navigator_core.getLoiterRadiusMeter());
|
||||
ASSERT_EQ(current.loiter_direction, 1);
|
||||
ASSERT_EQ(current.acceptance_radius, navigator_core.getHorAcceptanceRadiusMeter());
|
||||
ASSERT_EQ(current.cruising_speed, -1.0f);
|
||||
|
||||
uint64_t t_first = current.timestamp;
|
||||
|
||||
landed.landed = false;
|
||||
navigator_core.updateLandedState(landed);
|
||||
global_pos.alt += navigator_core.getRelativeTakeoffMinAltitudeMeter();
|
||||
navigator_core.updateGlobalPosition(global_pos);
|
||||
|
||||
takeoff.on_active();
|
||||
current = fake_navigator.get_position_setpoint_triplet()->current;
|
||||
|
||||
ASSERT_NE(t_first, current.timestamp);
|
||||
ASSERT_EQ(current.type, 2);
|
||||
|
||||
|
||||
|
||||
|
||||
}
|
||||
@ -11,7 +11,8 @@
|
||||
TEST(Navigator_and_RTL, interact_correctly)
|
||||
{
|
||||
Navigator n;
|
||||
RTL rtl(&n);
|
||||
NavigatorCore navigator_core;
|
||||
RTL rtl(&n, navigator_core);
|
||||
|
||||
|
||||
home_position_s home_pos{};
|
||||
|
||||
@ -52,8 +52,8 @@
|
||||
#include "navigator.h"
|
||||
#include "enginefailure.h"
|
||||
|
||||
EngineFailure::EngineFailure(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
EngineFailure::EngineFailure(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core),
|
||||
_ef_state(EF_STATE_NONE)
|
||||
{
|
||||
}
|
||||
@ -93,15 +93,15 @@ EngineFailure::set_ef_item()
|
||||
case EF_STATE_LOITERDOWN: {
|
||||
//XXX create mission item at ground (below?) here
|
||||
|
||||
_mission_item.lat = _navigator->get_global_position()->lat;
|
||||
_mission_item.lon = _navigator->get_global_position()->lon;
|
||||
_mission_item.lat = _navigator_core.getLatRad();
|
||||
_mission_item.lon = _navigator_core.getLonRad();
|
||||
_mission_item.altitude_is_relative = false;
|
||||
//XXX setting altitude to a very low value, evaluate other options
|
||||
_mission_item.altitude = _navigator->get_home_position()->alt - 1000.0f;
|
||||
_mission_item.altitude = _navigator_core.getHomeAltAMSLMeter() - 1000.0f;
|
||||
_mission_item.yaw = NAN;
|
||||
_mission_item.loiter_radius = _navigator->get_loiter_radius();
|
||||
_mission_item.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
_mission_item.nav_cmd = NAV_CMD_LOITER_UNLIMITED;
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
|
||||
|
||||
@ -47,7 +47,7 @@ class Navigator;
|
||||
class EngineFailure : public MissionBlock
|
||||
{
|
||||
public:
|
||||
EngineFailure(Navigator *navigator);
|
||||
EngineFailure(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~EngineFailure() = default;
|
||||
|
||||
void on_inactive() override;
|
||||
|
||||
@ -60,8 +60,8 @@ using namespace matrix;
|
||||
|
||||
constexpr float FollowTarget::_follow_position_matricies[4][9];
|
||||
|
||||
FollowTarget::FollowTarget(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
FollowTarget::FollowTarget(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core),
|
||||
ModuleParams(navigator)
|
||||
{
|
||||
_current_vel.zero();
|
||||
@ -134,7 +134,7 @@ void FollowTarget::on_active()
|
||||
|
||||
// get distance to target
|
||||
|
||||
map_projection_init(&target_ref, _navigator->get_global_position()->lat, _navigator->get_global_position()->lon);
|
||||
map_projection_init(&target_ref, _navigator_core.getLatRad(), _navigator_core.getLonRad());
|
||||
map_projection_project(&target_ref, _current_target_motion.lat, _current_target_motion.lon, &_target_distance(0),
|
||||
&_target_distance(1));
|
||||
|
||||
@ -200,12 +200,12 @@ void FollowTarget::on_active()
|
||||
// this really needs to control the yaw rate directly in the attitude pid controller
|
||||
// but seems to work ok for now since the yaw rate cannot be controlled directly in auto mode
|
||||
|
||||
_yaw_angle = get_bearing_to_next_waypoint(_navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon,
|
||||
_yaw_angle = get_bearing_to_next_waypoint(_navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad(),
|
||||
_current_target_motion.lat,
|
||||
_current_target_motion.lon);
|
||||
|
||||
_yaw_rate = wrap_pi((_yaw_angle - _navigator->get_local_position()->heading) / (dt_ms / 1000.0f));
|
||||
_yaw_rate = wrap_pi((_yaw_angle - _navigator_core.getTrueHeadingRad()) / (dt_ms / 1000.0f));
|
||||
|
||||
} else {
|
||||
_yaw_angle = _yaw_rate = NAN;
|
||||
@ -238,7 +238,7 @@ void FollowTarget::on_active()
|
||||
// 3 degrees of facing target
|
||||
|
||||
if (PX4_ISFINITE(_yaw_rate)) {
|
||||
if (fabsf(fabsf(_yaw_angle) - fabsf(_navigator->get_local_position()->heading)) < math::radians(3.0F)) {
|
||||
if (fabsf(fabsf(_yaw_angle) - fabsf(_navigator_core.getTrueHeadingRad())) < math::radians(3.0F)) {
|
||||
_yaw_rate = NAN;
|
||||
}
|
||||
}
|
||||
@ -298,8 +298,8 @@ void FollowTarget::on_active()
|
||||
|
||||
// for now set the target at the minimum height above the uav
|
||||
|
||||
target.lat = _navigator->get_global_position()->lat;
|
||||
target.lon = _navigator->get_global_position()->lon;
|
||||
target.lat = _navigator_core.getLatRad();
|
||||
target.lon = _navigator_core.getLonRad();
|
||||
target.alt = 0.0F;
|
||||
|
||||
set_follow_target_item(&_mission_item, _param_nav_min_ft_ht.get(), target, _yaw_angle);
|
||||
@ -376,7 +376,7 @@ void
|
||||
FollowTarget::set_follow_target_item(struct mission_item_s *item, float min_clearance, follow_target_s &target,
|
||||
float yaw)
|
||||
{
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
/* landed, don't takeoff, but switch to IDLE mode */
|
||||
item->nav_cmd = NAV_CMD_IDLE;
|
||||
|
||||
@ -387,7 +387,8 @@ FollowTarget::set_follow_target_item(struct mission_item_s *item, float min_clea
|
||||
/* use current target position */
|
||||
item->lat = target.lat;
|
||||
item->lon = target.lon;
|
||||
item->altitude = _navigator->get_home_position()->alt;
|
||||
item->altitude = _navigator_core.getHomeAltAMSLMeter();
|
||||
|
||||
|
||||
if (min_clearance > 8.0f) {
|
||||
item->altitude += min_clearance;
|
||||
@ -399,8 +400,8 @@ FollowTarget::set_follow_target_item(struct mission_item_s *item, float min_clea
|
||||
|
||||
item->altitude_is_relative = false;
|
||||
item->yaw = yaw;
|
||||
item->loiter_radius = _navigator->get_loiter_radius();
|
||||
item->acceptance_radius = _navigator->get_acceptance_radius();
|
||||
item->loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
item->acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
item->time_inside = 0.0f;
|
||||
item->autocontinue = false;
|
||||
item->origin = ORIGIN_ONBOARD;
|
||||
|
||||
@ -54,7 +54,7 @@ class FollowTarget : public MissionBlock, public ModuleParams
|
||||
{
|
||||
|
||||
public:
|
||||
FollowTarget(Navigator *navigator);
|
||||
FollowTarget(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~FollowTarget() = default;
|
||||
|
||||
void on_inactive() override;
|
||||
|
||||
@ -224,13 +224,13 @@ bool Geofence::isCloserThanMaxDistToHome(double lat, double lon, float altitude)
|
||||
{
|
||||
bool inside_fence = true;
|
||||
|
||||
if (isHomeRequired() && _navigator->home_position_valid()) {
|
||||
if (isHomeRequired() && _navigator->getCore().isHomeValid()) {
|
||||
|
||||
const float max_horizontal_distance = _param_gf_max_hor_dist.get();
|
||||
|
||||
const double home_lat = _navigator->get_home_position()->lat;
|
||||
const double home_lon = _navigator->get_home_position()->lon;
|
||||
const float home_alt = _navigator->get_home_position()->alt;
|
||||
const double home_lat = _navigator->getCore().getHomeLatRad();
|
||||
const double home_lon = _navigator->getCore().getHomeLonRad();
|
||||
const float home_alt = _navigator->getCore().getHomeAltAMSLMeter();
|
||||
|
||||
float dist_xy = -1.0f;
|
||||
float dist_z = -1.0f;
|
||||
@ -255,10 +255,10 @@ bool Geofence::isBelowMaxAltitude(float altitude)
|
||||
{
|
||||
bool inside_fence = true;
|
||||
|
||||
if (isHomeRequired() && _navigator->home_position_valid()) {
|
||||
if (isHomeRequired() && _navigator->getCore().isHomeValid()) {
|
||||
|
||||
const float max_vertical_distance = _param_gf_max_ver_dist.get();
|
||||
const float home_alt = _navigator->get_home_position()->alt;
|
||||
const float home_alt = _navigator->getCore().getHomeAltAMSLMeter();
|
||||
|
||||
float dist_z = altitude - home_alt;
|
||||
|
||||
|
||||
@ -52,8 +52,8 @@
|
||||
using matrix::Eulerf;
|
||||
using matrix::Quatf;
|
||||
|
||||
GpsFailure::GpsFailure(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
GpsFailure::GpsFailure(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core),
|
||||
ModuleParams(navigator)
|
||||
{
|
||||
}
|
||||
@ -92,7 +92,7 @@ GpsFailure::on_active()
|
||||
Quatf q(Eulerf(att_sp.roll_body, att_sp.pitch_body, 0.0f));
|
||||
q.copyTo(att_sp.q_d);
|
||||
|
||||
if (_navigator->get_vstatus()->is_vtol) {
|
||||
if (_navigator_core.isVTOL()) {
|
||||
_fw_virtual_att_sp_pub.publish(att_sp);
|
||||
|
||||
} else {
|
||||
|
||||
@ -51,7 +51,7 @@ class Navigator;
|
||||
class GpsFailure : public MissionBlock, public ModuleParams
|
||||
{
|
||||
public:
|
||||
GpsFailure(Navigator *navigator);
|
||||
GpsFailure(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~GpsFailure() = default;
|
||||
|
||||
void on_inactive() override;
|
||||
|
||||
@ -41,8 +41,8 @@
|
||||
#include "land.h"
|
||||
#include "navigator.h"
|
||||
|
||||
Land::Land(Navigator *navigator) :
|
||||
MissionBlock(navigator)
|
||||
Land::Land(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core)
|
||||
{
|
||||
}
|
||||
|
||||
@ -71,16 +71,16 @@ void
|
||||
Land::on_active()
|
||||
{
|
||||
/* for VTOL update landing location during back transition */
|
||||
if (_navigator->get_vstatus()->is_vtol &&
|
||||
_navigator->get_vstatus()->in_transition_mode) {
|
||||
if (_navigator_core.isVTOL() &&
|
||||
_navigator_core.getIsInTransitionMode()) {
|
||||
struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
pos_sp_triplet->current.lat = _navigator->get_global_position()->lat;
|
||||
pos_sp_triplet->current.lon = _navigator->get_global_position()->lon;
|
||||
pos_sp_triplet->current.lat = _navigator_core.getLatRad();
|
||||
pos_sp_triplet->current.lon = _navigator_core.getLonRad();
|
||||
_navigator->set_position_setpoint_triplet_updated();
|
||||
}
|
||||
|
||||
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
_navigator->get_mission_result()->finished = true;
|
||||
_navigator->set_mission_result_updated();
|
||||
set_idle_item(&_mission_item);
|
||||
|
||||
@ -46,7 +46,7 @@
|
||||
class Land : public MissionBlock
|
||||
{
|
||||
public:
|
||||
Land(Navigator *navigator);
|
||||
Land(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~Land() = default;
|
||||
|
||||
void on_activation() override;
|
||||
|
||||
@ -42,8 +42,8 @@
|
||||
#include "loiter.h"
|
||||
#include "navigator.h"
|
||||
|
||||
Loiter::Loiter(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
Loiter::Loiter(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core),
|
||||
ModuleParams(navigator)
|
||||
{
|
||||
}
|
||||
@ -73,7 +73,7 @@ Loiter::on_active()
|
||||
}
|
||||
|
||||
// reset the loiter position if we get disarmed
|
||||
if (_navigator->get_vstatus()->arming_state != vehicle_status_s::ARMING_STATE_ARMED) {
|
||||
if (_navigator_core.isNotArmed()) {
|
||||
_loiter_pos_set = false;
|
||||
}
|
||||
}
|
||||
@ -81,8 +81,8 @@ Loiter::on_active()
|
||||
void
|
||||
Loiter::set_loiter_position()
|
||||
{
|
||||
if (_navigator->get_vstatus()->arming_state != vehicle_status_s::ARMING_STATE_ARMED &&
|
||||
_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.isNotArmed() &&
|
||||
_navigator_core.getLanded()) {
|
||||
|
||||
// Not setting loiter position if disarmed and landed, instead mark the current
|
||||
// setpoint as invalid and idle (both, just to be sure).
|
||||
@ -101,7 +101,8 @@ Loiter::set_loiter_position()
|
||||
_loiter_pos_set = true;
|
||||
|
||||
// set current mission item to loiter
|
||||
set_loiter_item(&_mission_item, _navigator->get_loiter_min_alt());
|
||||
set_loiter_item(&_mission_item, _navigator_core.getRelativeLoiterMinAltitudeMeter());
|
||||
|
||||
|
||||
// convert mission item to current setpoint
|
||||
struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
@ -119,7 +120,7 @@ void
|
||||
Loiter::reposition()
|
||||
{
|
||||
// we can't reposition if we are not armed yet
|
||||
if (_navigator->get_vstatus()->arming_state != vehicle_status_s::ARMING_STATE_ARMED) {
|
||||
if (_navigator_core.isNotArmed()) {
|
||||
return;
|
||||
}
|
||||
|
||||
@ -131,10 +132,10 @@ Loiter::reposition()
|
||||
// convert mission item to current setpoint
|
||||
struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
pos_sp_triplet->current.velocity_valid = false;
|
||||
pos_sp_triplet->previous.yaw = _navigator->get_local_position()->heading;
|
||||
pos_sp_triplet->previous.lat = _navigator->get_global_position()->lat;
|
||||
pos_sp_triplet->previous.lon = _navigator->get_global_position()->lon;
|
||||
pos_sp_triplet->previous.alt = _navigator->get_global_position()->alt;
|
||||
pos_sp_triplet->previous.yaw = _navigator_core.getTrueHeadingRad();
|
||||
pos_sp_triplet->previous.lat = _navigator_core.getLatRad();
|
||||
pos_sp_triplet->previous.lon = _navigator_core.getLonRad();
|
||||
pos_sp_triplet->previous.alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
memcpy(&pos_sp_triplet->current, &rep->current, sizeof(rep->current));
|
||||
pos_sp_triplet->next.valid = false;
|
||||
|
||||
|
||||
@ -48,7 +48,7 @@
|
||||
class Loiter : public MissionBlock, public ModuleParams
|
||||
{
|
||||
public:
|
||||
Loiter(Navigator *navigator);
|
||||
Loiter(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~Loiter() = default;
|
||||
|
||||
void on_inactive() override;
|
||||
|
||||
@ -62,8 +62,8 @@
|
||||
|
||||
using namespace time_literals;
|
||||
|
||||
Mission::Mission(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
Mission::Mission(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core),
|
||||
ModuleParams(navigator)
|
||||
{
|
||||
}
|
||||
@ -83,7 +83,7 @@ Mission::on_inactive()
|
||||
}
|
||||
|
||||
/* Without home a mission can't be valid yet anyway, let's wait. */
|
||||
if (!_navigator->home_position_valid()) {
|
||||
if (!_navigator_core.isHomeValid()) {
|
||||
return;
|
||||
}
|
||||
|
||||
@ -131,7 +131,7 @@ Mission::on_inactive()
|
||||
}
|
||||
|
||||
/* require takeoff after non-loiter or landing */
|
||||
if (!_navigator->get_can_loiter_at_sp() || _navigator->get_land_detected()->landed) {
|
||||
if (!_navigator->get_can_loiter_at_sp() || _navigator_core.getLanded()) {
|
||||
_need_takeoff = true;
|
||||
}
|
||||
|
||||
@ -252,7 +252,7 @@ Mission::on_active()
|
||||
|
||||
/* see if we need to update the current yaw heading */
|
||||
if (!_param_mis_mnt_yaw_ctl.get()
|
||||
&& (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING)
|
||||
&& (_navigator_core.isRotaryWing())
|
||||
&& (_navigator->get_vroi().mode != vehicle_roi_s::ROI_NONE)
|
||||
&& !(_mission_item.nav_cmd == NAV_CMD_TAKEOFF
|
||||
|| _mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF
|
||||
@ -330,9 +330,9 @@ Mission::set_execution_mode(const uint8_t mode)
|
||||
case mission_result_s::MISSION_EXECUTION_MODE_FAST_FORWARD:
|
||||
if (mode == mission_result_s::MISSION_EXECUTION_MODE_REVERSE) {
|
||||
// command a transition if in vtol mc mode
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING &&
|
||||
_navigator->get_vstatus()->is_vtol &&
|
||||
!_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.isRotaryWing() &&
|
||||
_navigator_core.isVTOL() &&
|
||||
!_navigator_core.getLanded()) {
|
||||
|
||||
set_vtol_transition_item(&_mission_item, vtol_vehicle_status_s::VEHICLE_VTOL_STATE_FW);
|
||||
|
||||
@ -418,16 +418,16 @@ Mission::find_mission_land_start()
|
||||
_landing_start_lat = missionitem.lat;
|
||||
_landing_start_lon = missionitem.lon;
|
||||
_landing_start_alt = missionitem.altitude_is_relative ? missionitem.altitude +
|
||||
_navigator->get_home_position()->alt : missionitem.altitude;
|
||||
_navigator_core.getHomeAltAMSLMeter() : missionitem.altitude;
|
||||
_land_start_available = true;
|
||||
}
|
||||
|
||||
if (((missionitem.nav_cmd == NAV_CMD_VTOL_LAND) && _navigator->get_vstatus()->is_vtol) ||
|
||||
if (((missionitem.nav_cmd == NAV_CMD_VTOL_LAND) && _navigator_core.isVTOL()) ||
|
||||
(missionitem.nav_cmd == NAV_CMD_LAND)) {
|
||||
|
||||
_landing_lat = missionitem.lat;
|
||||
_landing_lon = missionitem.lon;
|
||||
_landing_alt = missionitem.altitude_is_relative ? missionitem.altitude + _navigator->get_home_position()->alt :
|
||||
_landing_alt = missionitem.altitude_is_relative ? missionitem.altitude + _navigator_core.getHomeAltAMSLMeter() :
|
||||
missionitem.altitude;
|
||||
|
||||
// don't have a valid land start yet, use the landing item itself then
|
||||
@ -529,7 +529,7 @@ Mission::update_mission()
|
||||
* TODO add a flag to mission_s which actually tracks if the position of the waypoint changed */
|
||||
if (((_mission.count != old_mission.count) ||
|
||||
(_mission.dataman_id != old_mission.dataman_id)) &&
|
||||
!_navigator->get_land_detected()->landed) {
|
||||
!_navigator_core.getLanded()) {
|
||||
_mission_waypoints_changed = true;
|
||||
}
|
||||
|
||||
@ -640,7 +640,7 @@ Mission::set_mission_items()
|
||||
/* no mission available or mission finished, switch to loiter */
|
||||
if (_mission_type != MISSION_TYPE_NONE) {
|
||||
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
mavlink_log_info(_navigator->get_mavlink_log_pub(),
|
||||
_mission_execution_mode == mission_result_s::MISSION_EXECUTION_MODE_REVERSE ? "Reverse Mission finished, landed" :
|
||||
"Mission finished, landed.");
|
||||
@ -661,7 +661,7 @@ Mission::set_mission_items()
|
||||
_mission_type = MISSION_TYPE_NONE;
|
||||
|
||||
/* set loiter mission item and ensure that there is a minimum clearance from home */
|
||||
set_loiter_item(&_mission_item, _navigator->get_takeoff_min_alt());
|
||||
set_loiter_item(&_mission_item, _navigator_core.getRelativeTakeoffMinAltitudeMeter());
|
||||
|
||||
/* update position setpoint triplet */
|
||||
position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
@ -683,7 +683,7 @@ Mission::set_mission_items()
|
||||
* https://en.wikipedia.org/wiki/Loiter_(aeronautics)
|
||||
*/
|
||||
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
/* landed, refusing to take off without a mission */
|
||||
mavlink_log_critical(_navigator->get_mavlink_log_pub(), "No valid mission available, refusing takeoff.");
|
||||
|
||||
@ -711,7 +711,7 @@ Mission::set_mission_items()
|
||||
case mission_result_s::MISSION_EXECUTION_MODE_NORMAL:
|
||||
case mission_result_s::MISSION_EXECUTION_MODE_FAST_FORWARD: {
|
||||
/* force vtol land */
|
||||
if (_navigator->force_vtol() && _mission_item.nav_cmd == NAV_CMD_LAND) {
|
||||
if (_navigator_core.forceVTOL() && _mission_item.nav_cmd == NAV_CMD_LAND) {
|
||||
_mission_item.nav_cmd = NAV_CMD_VTOL_LAND;
|
||||
}
|
||||
|
||||
@ -733,13 +733,13 @@ Mission::set_mission_items()
|
||||
float takeoff_alt = calculate_takeoff_altitude(&_mission_item);
|
||||
|
||||
mavlink_log_info(_navigator->get_mavlink_log_pub(), "Takeoff to %.1f meters above home.",
|
||||
(double)(takeoff_alt - _navigator->get_home_position()->alt));
|
||||
(double)(takeoff_alt - _navigator_core.getHomeAltAMSLMeter()));
|
||||
|
||||
_mission_item.nav_cmd = NAV_CMD_TAKEOFF;
|
||||
_mission_item.lat = _navigator->get_global_position()->lat;
|
||||
_mission_item.lon = _navigator->get_global_position()->lon;
|
||||
_mission_item.lat = _navigator_core.getLatRad();
|
||||
_mission_item.lon = _navigator_core.getLonRad();
|
||||
/* hold heading for takeoff items */
|
||||
_mission_item.yaw = _navigator->get_local_position()->heading;
|
||||
_mission_item.yaw = _navigator_core.getTrueHeadingRad();
|
||||
_mission_item.altitude = takeoff_alt;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.autocontinue = true;
|
||||
@ -748,7 +748,7 @@ Mission::set_mission_items()
|
||||
} else if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF
|
||||
&& _work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& new_work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
&& _navigator_core.isRotaryWing()) {
|
||||
|
||||
/* if there is no need to do a takeoff but we have a takeoff item, treat is as waypoint */
|
||||
_mission_item.nav_cmd = NAV_CMD_WAYPOINT;
|
||||
@ -759,7 +759,7 @@ Mission::set_mission_items()
|
||||
&& _work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& new_work_item_type == WORK_ITEM_TYPE_DEFAULT) {
|
||||
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
if (_navigator_core.isRotaryWing()) {
|
||||
/* haven't transitioned yet, trigger vtol takeoff logic below */
|
||||
_work_item_type = WORK_ITEM_TYPE_TAKEOFF;
|
||||
|
||||
@ -786,15 +786,15 @@ Mission::set_mission_items()
|
||||
if (_mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF &&
|
||||
_work_item_type == WORK_ITEM_TYPE_TAKEOFF &&
|
||||
new_work_item_type == WORK_ITEM_TYPE_DEFAULT &&
|
||||
_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING &&
|
||||
!_navigator->get_land_detected()->landed) {
|
||||
_navigator_core.isRotaryWing() &&
|
||||
!_navigator_core.getLanded()) {
|
||||
|
||||
/* disable weathervane before front transition for allowing yaw to align */
|
||||
pos_sp_triplet->current.disable_weather_vane = true;
|
||||
|
||||
/* set yaw setpoint to heading of VTOL_TAKEOFF wp against current position */
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(
|
||||
_navigator->get_global_position()->lat, _navigator->get_global_position()->lon,
|
||||
_navigator_core.getLatRad(), _navigator_core.getLonRad(),
|
||||
_mission_item.lat, _mission_item.lon);
|
||||
|
||||
_mission_item.force_heading = true;
|
||||
@ -802,15 +802,15 @@ Mission::set_mission_items()
|
||||
new_work_item_type = WORK_ITEM_TYPE_ALIGN;
|
||||
|
||||
/* set position setpoint to current while aligning */
|
||||
_mission_item.lat = _navigator->get_global_position()->lat;
|
||||
_mission_item.lon = _navigator->get_global_position()->lon;
|
||||
_mission_item.lat = _navigator_core.getLatRad();
|
||||
_mission_item.lon = _navigator_core.getLonRad();
|
||||
}
|
||||
|
||||
/* heading is aligned now, prepare transition */
|
||||
if (_mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF &&
|
||||
_work_item_type == WORK_ITEM_TYPE_ALIGN &&
|
||||
_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING &&
|
||||
!_navigator->get_land_detected()->landed) {
|
||||
_navigator_core.isRotaryWing() &&
|
||||
!_navigator_core.getLanded()) {
|
||||
|
||||
/* re-enable weather vane again after alignment */
|
||||
pos_sp_triplet->current.disable_weather_vane = false;
|
||||
@ -821,7 +821,7 @@ Mission::set_mission_items()
|
||||
}
|
||||
|
||||
set_vtol_transition_item(&_mission_item, vtol_vehicle_status_s::VEHICLE_VTOL_STATE_FW);
|
||||
_mission_item.yaw = _navigator->get_local_position()->heading;
|
||||
_mission_item.yaw = _navigator_core.getTrueHeadingRad();
|
||||
|
||||
/* set position setpoint to target during the transition */
|
||||
generate_waypoint_from_heading(&pos_sp_triplet->current, _mission_item.yaw);
|
||||
@ -842,7 +842,7 @@ Mission::set_mission_items()
|
||||
if (_mission_item.nav_cmd == NAV_CMD_VTOL_LAND
|
||||
&& (_work_item_type == WORK_ITEM_TYPE_DEFAULT || _work_item_type == WORK_ITEM_TYPE_TRANSITON_AFTER_TAKEOFF)
|
||||
&& new_work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& !_navigator->get_land_detected()->landed) {
|
||||
&& !_navigator_core.getLanded()) {
|
||||
|
||||
new_work_item_type = WORK_ITEM_TYPE_MOVE_TO_LAND;
|
||||
|
||||
@ -850,7 +850,7 @@ Mission::set_mission_items()
|
||||
mission_item_next_position = _mission_item;
|
||||
has_next_position_item = true;
|
||||
|
||||
float altitude = _navigator->get_global_position()->alt;
|
||||
float altitude = _navigator_core.getAltitudeAMSLMeters();
|
||||
|
||||
if (pos_sp_triplet->current.valid && pos_sp_triplet->current.type == position_setpoint_s::SETPOINT_TYPE_POSITION) {
|
||||
altitude = pos_sp_triplet->current.alt;
|
||||
@ -868,11 +868,11 @@ Mission::set_mission_items()
|
||||
if (_mission_item.nav_cmd == NAV_CMD_VTOL_LAND
|
||||
&& _work_item_type == WORK_ITEM_TYPE_MOVE_TO_LAND
|
||||
&& new_work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING
|
||||
&& !_navigator->get_land_detected()->landed) {
|
||||
&& _navigator_core.isFixedWing()
|
||||
&& !_navigator_core.getLanded()) {
|
||||
|
||||
set_vtol_transition_item(&_mission_item, vtol_vehicle_status_s::VEHICLE_VTOL_STATE_MC);
|
||||
_mission_item.altitude = _navigator->get_global_position()->alt;
|
||||
_mission_item.altitude = _navigator_core.getAltitudeAMSLMeters();
|
||||
_mission_item.altitude_is_relative = false;
|
||||
|
||||
new_work_item_type = WORK_ITEM_TYPE_MOVE_TO_LAND_AFTER_TRANSITION;
|
||||
@ -901,7 +901,7 @@ Mission::set_mission_items()
|
||||
* XXX: We might want to change that at some point if it is clear to the user
|
||||
* what the altitude means on this waypoint type.
|
||||
*/
|
||||
float altitude = _navigator->get_global_position()->alt;
|
||||
float altitude = _navigator_core.getAltitudeAMSLMeters();
|
||||
|
||||
if (pos_sp_triplet->current.valid
|
||||
&& pos_sp_triplet->current.type == position_setpoint_s::SETPOINT_TYPE_POSITION) {
|
||||
@ -1001,8 +1001,8 @@ Mission::set_mission_items()
|
||||
if (_mission_item.nav_cmd == NAV_CMD_DO_VTOL_TRANSITION
|
||||
&& _work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& new_work_item_type == WORK_ITEM_TYPE_DEFAULT
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
||||
&& !_navigator->get_land_detected()->landed
|
||||
&& _navigator_core.isRotaryWing()
|
||||
&& !_navigator_core.getLanded()
|
||||
&& has_next_position_item) {
|
||||
|
||||
/* disable weathervane before front transition for allowing yaw to align */
|
||||
@ -1134,9 +1134,8 @@ Mission::set_mission_items()
|
||||
}
|
||||
|
||||
} else {
|
||||
/* allow the vehicle to decelerate before reaching a wp with a hold time */
|
||||
const bool brake_for_hold = _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
||||
&& get_time_inside(_mission_item) > FLT_EPSILON;
|
||||
const bool brake_for_hold = _navigator_core.isRotaryWing()
|
||||
&& get_time_inside(_mission_item) > FLT_EPSILON; //allow the vehicle to decelerate before reaching a wp with a hold time
|
||||
|
||||
if (_mission_item.autocontinue && !brake_for_hold) {
|
||||
/* try to process next mission item */
|
||||
@ -1162,19 +1161,19 @@ Mission::set_mission_items()
|
||||
bool
|
||||
Mission::do_need_vertical_takeoff()
|
||||
{
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
if (_navigator_core.isRotaryWing()) {
|
||||
|
||||
float takeoff_alt = calculate_takeoff_altitude(&_mission_item);
|
||||
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
/* force takeoff if landed (additional protection) */
|
||||
_need_takeoff = true;
|
||||
|
||||
} else if (_navigator->get_global_position()->alt > takeoff_alt - _navigator->get_altitude_acceptance_radius()) {
|
||||
} else if (_navigator_core.getAltitudeAMSLMeters() > takeoff_alt - _navigator_core.getAltAcceptanceRadiusMeter()) {
|
||||
/* if in-air and already above takeoff height, don't do takeoff */
|
||||
_need_takeoff = false;
|
||||
|
||||
} else if (_navigator->get_global_position()->alt <= takeoff_alt - _navigator->get_altitude_acceptance_radius()
|
||||
} else if (_navigator_core.getAltitudeAMSLMeters() <= takeoff_alt - _navigator_core.getAltAcceptanceRadiusMeter()
|
||||
&& (_mission_item.nav_cmd == NAV_CMD_TAKEOFF
|
||||
|| _mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF)) {
|
||||
/* if in-air but below takeoff height and we have a takeoff item */
|
||||
@ -1200,13 +1199,13 @@ Mission::do_need_vertical_takeoff()
|
||||
bool
|
||||
Mission::do_need_move_to_land()
|
||||
{
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
||||
if (_navigator_core.isRotaryWing()
|
||||
&& (_mission_item.nav_cmd == NAV_CMD_LAND || _mission_item.nav_cmd == NAV_CMD_VTOL_LAND)) {
|
||||
|
||||
float d_current = get_distance_to_next_waypoint(_mission_item.lat, _mission_item.lon,
|
||||
_navigator->get_global_position()->lat, _navigator->get_global_position()->lon);
|
||||
_navigator_core.getLatRad(), _navigator_core.getLonRad());
|
||||
|
||||
return d_current > _navigator->get_acceptance_radius();
|
||||
return d_current > _navigator_core.getAcceptanceRadiusMeter();
|
||||
}
|
||||
|
||||
return false;
|
||||
@ -1215,13 +1214,13 @@ Mission::do_need_move_to_land()
|
||||
bool
|
||||
Mission::do_need_move_to_takeoff()
|
||||
{
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
||||
if (_navigator_core.isRotaryWing()
|
||||
&& _mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF) {
|
||||
|
||||
float d_current = get_distance_to_next_waypoint(_mission_item.lat, _mission_item.lon,
|
||||
_navigator->get_global_position()->lat, _navigator->get_global_position()->lon);
|
||||
_navigator_core.getLatRad(), _navigator_core.getLonRad());
|
||||
|
||||
return d_current > _navigator->get_acceptance_radius();
|
||||
return d_current > _navigator_core.getAcceptanceRadiusMeter();
|
||||
}
|
||||
|
||||
return false;
|
||||
@ -1236,9 +1235,9 @@ Mission::copy_position_if_valid(struct mission_item_s *mission_item, struct posi
|
||||
mission_item->altitude = setpoint->alt;
|
||||
|
||||
} else {
|
||||
mission_item->lat = _navigator->get_global_position()->lat;
|
||||
mission_item->lon = _navigator->get_global_position()->lon;
|
||||
mission_item->altitude = _navigator->get_global_position()->alt;
|
||||
mission_item->lat = _navigator_core.getLatRad();
|
||||
mission_item->lon = _navigator_core.getLonRad();
|
||||
mission_item->altitude = _navigator_core.getAltitudeAMSLMeters();
|
||||
}
|
||||
|
||||
mission_item->altitude_is_relative = false;
|
||||
@ -1253,7 +1252,7 @@ Mission::set_align_mission_item(struct mission_item_s *mission_item, struct miss
|
||||
mission_item->autocontinue = true;
|
||||
mission_item->time_inside = 0.0f;
|
||||
mission_item->yaw = get_bearing_to_next_waypoint(
|
||||
_navigator->get_global_position()->lat, _navigator->get_global_position()->lon,
|
||||
_navigator_core.getLatRad(), _navigator_core.getLonRad(),
|
||||
mission_item_next->lat, mission_item_next->lon);
|
||||
mission_item->force_heading = true;
|
||||
}
|
||||
@ -1265,11 +1264,13 @@ Mission::calculate_takeoff_altitude(struct mission_item_s *mission_item)
|
||||
float takeoff_alt = get_absolute_altitude_for_item(*mission_item);
|
||||
|
||||
/* takeoff to at least MIS_TAKEOFF_ALT above home/ground, even if first waypoint is lower */
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
takeoff_alt = fmaxf(takeoff_alt, _navigator->get_global_position()->alt + _navigator->get_takeoff_min_alt());
|
||||
if (_navigator_core.getLanded()) {
|
||||
takeoff_alt = fmaxf(takeoff_alt, _navigator_core.getAltitudeAMSLMeters() +
|
||||
_navigator_core.getRelativeTakeoffMinAltitudeMeter());
|
||||
|
||||
} else {
|
||||
takeoff_alt = fmaxf(takeoff_alt, _navigator->get_home_position()->alt + _navigator->get_takeoff_min_alt());
|
||||
takeoff_alt = fmaxf(takeoff_alt, _navigator_core.getHomeAltAMSLMeter() +
|
||||
_navigator_core.getRelativeTakeoffMinAltitudeMeter());
|
||||
}
|
||||
|
||||
return takeoff_alt;
|
||||
@ -1284,11 +1285,11 @@ Mission::heading_sp_update()
|
||||
// Only update if current triplet is valid
|
||||
if (pos_sp_triplet->current.valid) {
|
||||
|
||||
double point_from_latlon[2] = { _navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon
|
||||
double point_from_latlon[2] = { _navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad()
|
||||
};
|
||||
double point_to_latlon[2] = { _navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon
|
||||
double point_to_latlon[2] = { _navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad()
|
||||
};
|
||||
float yaw_offset = 0.0f;
|
||||
|
||||
@ -1327,7 +1328,7 @@ Mission::heading_sp_update()
|
||||
float d_current = get_distance_to_next_waypoint(point_from_latlon[0],
|
||||
point_from_latlon[1], point_to_latlon[0], point_to_latlon[1]);
|
||||
|
||||
if (d_current > _navigator->get_acceptance_radius()) {
|
||||
if (d_current > _navigator_core.getAcceptanceRadiusMeter()) {
|
||||
float yaw = matrix::wrap_pi(
|
||||
get_bearing_to_next_waypoint(point_from_latlon[0],
|
||||
point_from_latlon[1], point_to_latlon[0],
|
||||
@ -1339,7 +1340,7 @@ Mission::heading_sp_update()
|
||||
|
||||
} else {
|
||||
if (!pos_sp_triplet->current.yaw_valid) {
|
||||
_mission_item.yaw = _navigator->get_local_position()->heading;
|
||||
_mission_item.yaw = _navigator_core.getTrueHeadingRad();
|
||||
pos_sp_triplet->current.yaw = _mission_item.yaw;
|
||||
pos_sp_triplet->current.yaw_valid = true;
|
||||
}
|
||||
@ -1383,15 +1384,15 @@ Mission::do_abort_landing()
|
||||
// loiter at the larger of MIS_LTRMIN_ALT above the landing point
|
||||
// or 2 * FW_CLMBOUT_DIFF above the current altitude
|
||||
const float alt_landing = get_absolute_altitude_for_item(_mission_item);
|
||||
const float alt_sp = math::max(alt_landing + _navigator->get_loiter_min_alt(),
|
||||
_navigator->get_global_position()->alt + 20.0f);
|
||||
const float alt_sp = math::max(alt_landing + _navigator_core.getRelativeLoiterMinAltitudeMeter(),
|
||||
_navigator_core.getAltitudeAMSLMeters() + 20.0f);
|
||||
|
||||
// turn current landing waypoint into an indefinite loiter
|
||||
_mission_item.nav_cmd = NAV_CMD_LOITER_UNLIMITED;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.altitude = alt_sp;
|
||||
_mission_item.loiter_radius = _navigator->get_loiter_radius();
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.autocontinue = false;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
|
||||
@ -1659,7 +1660,7 @@ Mission::set_current_mission_item()
|
||||
void
|
||||
Mission::check_mission_valid(bool force)
|
||||
{
|
||||
if ((!_home_inited && _navigator->home_position_valid()) || force) {
|
||||
if ((!_home_inited && _navigator_core.isHomeValid()) || force) {
|
||||
|
||||
MissionFeasibilityChecker _missionFeasibilityChecker(_navigator);
|
||||
|
||||
@ -1672,7 +1673,7 @@ Mission::check_mission_valid(bool force)
|
||||
_navigator->get_mission_result()->seq_total = _mission.count;
|
||||
_navigator->increment_mission_instance_count();
|
||||
_navigator->set_mission_result_updated();
|
||||
_home_inited = _navigator->home_position_valid();
|
||||
_home_inited = _navigator_core.isHomeValid();
|
||||
|
||||
// find and store landing start marker (if available)
|
||||
find_mission_land_start();
|
||||
@ -1733,7 +1734,7 @@ bool
|
||||
Mission::need_to_reset_mission()
|
||||
{
|
||||
/* reset mission state when disarmed */
|
||||
if (_navigator->get_vstatus()->arming_state != vehicle_status_s::ARMING_STATE_ARMED && _need_mission_reset) {
|
||||
if (_navigator_core.isNotArmed() && _need_mission_reset) {
|
||||
_need_mission_reset = false;
|
||||
return true;
|
||||
}
|
||||
@ -1745,7 +1746,7 @@ void
|
||||
Mission::generate_waypoint_from_heading(struct position_setpoint_s *setpoint, float yaw)
|
||||
{
|
||||
waypoint_from_heading_and_distance(
|
||||
_navigator->get_global_position()->lat, _navigator->get_global_position()->lon,
|
||||
_navigator_core.getLatRad(), _navigator_core.getLonRad(),
|
||||
yaw, 1000000.0f,
|
||||
&(setpoint->lat), &(setpoint->lon));
|
||||
setpoint->type = position_setpoint_s::SETPOINT_TYPE_POSITION;
|
||||
@ -1773,13 +1774,13 @@ Mission::index_closest_mission_item() const
|
||||
if (item_contains_position(missionitem)) {
|
||||
// do not consider land waypoints for a fw
|
||||
if (!((missionitem.nav_cmd == NAV_CMD_LAND) &&
|
||||
(_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING) &&
|
||||
(!_navigator->get_vstatus()->is_vtol))) {
|
||||
(_navigator_core.isFixedWing()) &&
|
||||
(!_navigator_core.isVTOL()))) {
|
||||
float dist = get_distance_to_point_global_wgs84(missionitem.lat, missionitem.lon,
|
||||
get_absolute_altitude_for_item(missionitem),
|
||||
_navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon,
|
||||
_navigator->get_global_position()->alt,
|
||||
_navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad(),
|
||||
_navigator_core.getAltitudeAMSLMeters(),
|
||||
&dist_xy, &dist_z);
|
||||
|
||||
if (dist < min_dist) {
|
||||
@ -1793,12 +1794,12 @@ Mission::index_closest_mission_item() const
|
||||
// for mission reverse also consider the home position
|
||||
if (_mission_execution_mode == mission_result_s::MISSION_EXECUTION_MODE_REVERSE) {
|
||||
float dist = get_distance_to_point_global_wgs84(
|
||||
_navigator->get_home_position()->lat,
|
||||
_navigator->get_home_position()->lon,
|
||||
_navigator->get_home_position()->alt,
|
||||
_navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon,
|
||||
_navigator->get_global_position()->alt,
|
||||
_navigator_core.getHomeLatRad(),
|
||||
_navigator_core.getHomeLonRad(),
|
||||
_navigator_core.getHomeAltAMSLMeter(),
|
||||
_navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad(),
|
||||
_navigator_core.getAltitudeAMSLMeters(),
|
||||
&dist_xy, &dist_z);
|
||||
|
||||
if (dist < min_dist) {
|
||||
|
||||
@ -69,7 +69,7 @@ class Navigator;
|
||||
class Mission : public MissionBlock, public ModuleParams
|
||||
{
|
||||
public:
|
||||
Mission(Navigator *navigator);
|
||||
Mission(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~Mission() override = default;
|
||||
|
||||
void on_inactive() override;
|
||||
|
||||
@ -56,14 +56,15 @@
|
||||
|
||||
using matrix::wrap_pi;
|
||||
|
||||
MissionBlock::MissionBlock(Navigator *navigator) :
|
||||
NavigatorMode(navigator)
|
||||
MissionBlock::MissionBlock(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
NavigatorMode(navigator),
|
||||
_navigator_core(navigator_core)
|
||||
{
|
||||
_mission_item.lat = (double)NAN;
|
||||
_mission_item.lon = (double)NAN;
|
||||
_mission_item.yaw = NAN;
|
||||
_mission_item.loiter_radius = _navigator->get_loiter_radius();
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
//_mission_item.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
//_mission_item.acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = 0.0f;
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -80,7 +81,7 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
case NAV_CMD_LAND: /* fall through */
|
||||
case NAV_CMD_VTOL_LAND:
|
||||
return _navigator->get_land_detected()->landed;
|
||||
return _navigator_core.getLanded();
|
||||
|
||||
case NAV_CMD_IDLE: /* fall through */
|
||||
case NAV_CMD_LOITER_UNLIMITED:
|
||||
@ -114,11 +115,11 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
if (int(_mission_item.params[0]) == 3) {
|
||||
// transition to RW requested, only accept waypoint if vehicle state has changed accordingly
|
||||
return _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
|
||||
return _navigator_core.isRotaryWing();
|
||||
|
||||
} else if (int(_mission_item.params[0]) == 4) {
|
||||
// transition to FW requested, only accept waypoint if vehicle state has changed accordingly
|
||||
return _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
|
||||
return _navigator_core.isFixedWing();
|
||||
|
||||
} else {
|
||||
// invalid vtol transition request
|
||||
@ -136,8 +137,7 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
hrt_abstime now = hrt_absolute_time();
|
||||
|
||||
if (!_navigator->get_land_detected()->landed && !_waypoint_position_reached) {
|
||||
|
||||
if (!_navigator_core.getLanded() && !_waypoint_position_reached) {
|
||||
float dist = -1.0f;
|
||||
float dist_xy = -1.0f;
|
||||
float dist_z = -1.0f;
|
||||
@ -145,23 +145,22 @@ MissionBlock::is_mission_item_reached()
|
||||
const float mission_item_altitude_amsl = get_absolute_altitude_for_item(_mission_item);
|
||||
|
||||
dist = get_distance_to_point_global_wgs84(_mission_item.lat, _mission_item.lon, mission_item_altitude_amsl,
|
||||
_navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon,
|
||||
_navigator->get_global_position()->alt,
|
||||
_navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad(),
|
||||
_navigator_core.getAltitudeAMSLMeters(),
|
||||
&dist_xy, &dist_z);
|
||||
|
||||
if ((_mission_item.nav_cmd == NAV_CMD_TAKEOFF || _mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF)
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
|
||||
&& _navigator_core.isRotaryWing()) {
|
||||
/* We want to avoid the edge case where the acceptance radius is bigger or equal than
|
||||
* the altitude of the takeoff waypoint above home. Otherwise, we do not really follow
|
||||
* take-off procedures like leaving the landing gear down. */
|
||||
|
||||
float takeoff_alt = _mission_item.altitude_is_relative ?
|
||||
_mission_item.altitude :
|
||||
(_mission_item.altitude - _navigator->get_home_position()->alt);
|
||||
(_mission_item.altitude - _navigator_core.getHomeAltAMSLMeter());
|
||||
|
||||
float altitude_acceptance_radius = _navigator->get_altitude_acceptance_radius();
|
||||
float altitude_acceptance_radius = _navigator_core.getAltAcceptanceRadMeter();
|
||||
|
||||
/* It should be safe to just use half of the takoeff_alt as an acceptance radius. */
|
||||
if (takeoff_alt > 0 && takeoff_alt < altitude_acceptance_radius) {
|
||||
@ -169,26 +168,26 @@ MissionBlock::is_mission_item_reached()
|
||||
}
|
||||
|
||||
/* require only altitude for takeoff for multicopter */
|
||||
if (_navigator->get_global_position()->alt >
|
||||
if (_navigator_core.getAltitudeAMSLMeters() >
|
||||
mission_item_altitude_amsl - altitude_acceptance_radius) {
|
||||
_waypoint_position_reached = true;
|
||||
}
|
||||
|
||||
} else if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROVER) {
|
||||
&& _navigator_core.isRover()) {
|
||||
/* for takeoff mission items use the parameter for the takeoff acceptance radius */
|
||||
if (dist_xy >= 0.0f && dist_xy <= _navigator->get_acceptance_radius()) {
|
||||
if (dist_xy >= 0.0f && dist_xy <= _navigator_core.getHorAcceptanceRadiusMeter()) {
|
||||
_waypoint_position_reached = true;
|
||||
}
|
||||
|
||||
} else if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF) {
|
||||
/* for takeoff mission items use the parameter for the takeoff acceptance radius */
|
||||
if (dist >= 0.0f && dist <= _navigator->get_acceptance_radius()
|
||||
&& dist_z <= _navigator->get_altitude_acceptance_radius()) {
|
||||
if (dist >= 0.0f && dist <= _navigator_core.getHorAcceptanceRadiusMeter()
|
||||
&& dist_z <= _navigator_core.getAltAcceptanceRadMeter()) {
|
||||
_waypoint_position_reached = true;
|
||||
}
|
||||
|
||||
} else if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING &&
|
||||
} else if (_navigator_core.isFixedWing() &&
|
||||
(_mission_item.nav_cmd == NAV_CMD_LOITER_UNLIMITED ||
|
||||
_mission_item.nav_cmd == NAV_CMD_LOITER_TIME_LIMIT)) {
|
||||
|
||||
@ -200,8 +199,8 @@ MissionBlock::is_mission_item_reached()
|
||||
*/
|
||||
|
||||
// check if within loiter radius around wp, if yes then set altitude sp to mission item
|
||||
if (dist >= 0.0f && dist_xy <= (_navigator->get_acceptance_radius() + fabsf(_mission_item.loiter_radius))
|
||||
&& dist_z <= _navigator->get_altitude_acceptance_radius()) {
|
||||
if (dist >= 0.0f && dist_xy <= (_navigator_core.getHorAcceptanceRadiusMeter() + fabsf(_mission_item.loiter_radius))
|
||||
&& dist_z <= _navigator_core.getAltAcceptanceRadMeter()) {
|
||||
|
||||
_waypoint_position_reached = true;
|
||||
}
|
||||
@ -216,22 +215,22 @@ MissionBlock::is_mission_item_reached()
|
||||
dist_z = -1.0f;
|
||||
|
||||
dist = get_distance_to_point_global_wgs84(_mission_item.lat, _mission_item.lon, curr_sp->alt,
|
||||
_navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon,
|
||||
_navigator->get_global_position()->alt,
|
||||
_navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad(),
|
||||
_navigator_core.getAltitudeAMSLMeters(),
|
||||
&dist_xy, &dist_z);
|
||||
|
||||
// check if within loiter radius around wp, if yes then set altitude sp to mission item
|
||||
if (dist >= 0.0f && dist_xy <= (_navigator->get_acceptance_radius() + fabsf(_mission_item.loiter_radius))
|
||||
&& dist_z <= _navigator->get_default_altitude_acceptance_radius()) {
|
||||
if (dist >= 0.0f && dist_xy <= (_navigator_core.getHorAcceptanceRadiusMeter() + fabsf(_mission_item.loiter_radius))
|
||||
&& dist_z <= _navigator_core.getDefaultAltAcceptanceRadiusMeter()) {
|
||||
|
||||
curr_sp->alt = mission_item_altitude_amsl;
|
||||
curr_sp->type = position_setpoint_s::SETPOINT_TYPE_LOITER;
|
||||
_navigator->set_position_setpoint_triplet_updated();
|
||||
}
|
||||
|
||||
} else if (dist >= 0.f && dist_xy <= (_navigator->get_acceptance_radius() + fabsf(_mission_item.loiter_radius))
|
||||
&& dist_z <= _navigator->get_altitude_acceptance_radius()) {
|
||||
} else if (dist >= 0.f && dist_xy <= (_navigator_core.getAcceptanceRadiusMeter() + fabsf(_mission_item.loiter_radius))
|
||||
&& dist_z <= _navigator_core.getAltAcceptanceRadiusMeter()) {
|
||||
// loitering, check if new altitude is reached, while still also having check on position
|
||||
|
||||
_waypoint_position_reached = true;
|
||||
@ -257,7 +256,7 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
// system position
|
||||
matrix::Vector2f vehicle_pos;
|
||||
map_projection_project(&ref_pos, _navigator->get_global_position()->lat, _navigator->get_global_position()->lon,
|
||||
map_projection_project(&ref_pos, _navigator_core.getLatRad(), _navigator_core.getLonRad(),
|
||||
&vehicle_pos(0), &vehicle_pos(1));
|
||||
const float dot_product = vehicle_pos.dot(gate_to_curr_sp.normalized());
|
||||
|
||||
@ -279,14 +278,14 @@ MissionBlock::is_mission_item_reached()
|
||||
} else {
|
||||
/*normal mission items */
|
||||
|
||||
float mission_acceptance_radius = _navigator->get_acceptance_radius();
|
||||
float mission_acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
|
||||
/* for vtol back transition calculate acceptance radius based on time and ground speed */
|
||||
if (_mission_item.vtol_back_transition
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING) {
|
||||
&& _navigator_core.isFixedWing()) {
|
||||
|
||||
float velocity = sqrtf(_navigator->get_local_position()->vx * _navigator->get_local_position()->vx +
|
||||
_navigator->get_local_position()->vy * _navigator->get_local_position()->vy);
|
||||
float velocity = sqrtf(_navigator_core.getVelNorthMPS() * _navigator_core.getVelNorthMPS() +
|
||||
_navigator_core.getVelEastMPS() * _navigator_core.getVelEastMPS());
|
||||
|
||||
const float back_trans_dec = _navigator->get_vtol_back_trans_deceleration();
|
||||
const float reverse_delay = _navigator->get_vtol_reverse_delay();
|
||||
@ -299,7 +298,7 @@ MissionBlock::is_mission_item_reached()
|
||||
}
|
||||
|
||||
if (dist_xy >= 0.0f && dist_xy <= mission_acceptance_radius
|
||||
&& dist_z <= _navigator->get_altitude_acceptance_radius()) {
|
||||
&& dist_z <= _navigator_core.getAltAcceptanceRadiusMeter()) {
|
||||
_waypoint_position_reached = true;
|
||||
}
|
||||
}
|
||||
@ -310,7 +309,7 @@ MissionBlock::is_mission_item_reached()
|
||||
}
|
||||
|
||||
// consider yaw reached for non-rotary wing vehicles (such as fixed-wing)
|
||||
if (_navigator->get_vstatus()->vehicle_type != vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
if (!_navigator_core.isRotaryWing()) {
|
||||
_waypoint_yaw_reached = true;
|
||||
}
|
||||
}
|
||||
@ -319,22 +318,22 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
if (_waypoint_position_reached && !_waypoint_yaw_reached) {
|
||||
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
||||
if (_navigator_core.isRotaryWing()
|
||||
&& PX4_ISFINITE(_navigator->get_yaw_acceptance(_mission_item.yaw))) {
|
||||
|
||||
const float yaw_err = wrap_pi(_mission_item.yaw - _navigator->get_local_position()->heading);
|
||||
const float yaw_err = wrap_pi(_mission_item.yaw - _navigator_core.getTrueHeadingRad());
|
||||
|
||||
/* accept yaw if reached or if timeout is set in which case we ignore not forced headings */
|
||||
if (fabsf(yaw_err) < _navigator->get_yaw_threshold()
|
||||
|| (_navigator->get_yaw_timeout() >= FLT_EPSILON && !_mission_item.force_heading)) {
|
||||
if (fabsf(yaw_err) < _navigator_core.getWaypointHeadingAcceptanceRad()
|
||||
|| (_navigator_core.getWaypointHeadingTimeoutSeconds() >= FLT_EPSILON && !_mission_item.force_heading)) {
|
||||
|
||||
_waypoint_yaw_reached = true;
|
||||
}
|
||||
|
||||
/* if heading needs to be reached, the timeout is enabled and we don't make it, abort mission */
|
||||
if (!_waypoint_yaw_reached && _mission_item.force_heading &&
|
||||
(_navigator->get_yaw_timeout() >= FLT_EPSILON) &&
|
||||
(now - _time_wp_reached >= (hrt_abstime)_navigator->get_yaw_timeout() * 1e6f)) {
|
||||
(_navigator_core.getWaypointHeadingTimeoutSeconds() >= FLT_EPSILON) &&
|
||||
(now - _time_wp_reached >= (hrt_abstime)_navigator_core.getWaypointHeadingTimeoutSeconds() * 1e6f)) {
|
||||
|
||||
_navigator->set_mission_failure("unable to reach heading within timeout");
|
||||
}
|
||||
@ -365,7 +364,7 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
/* enforce exit heading if in FW, the next wp is valid, the vehicle is currently loitering and either having force_heading set,
|
||||
or if loitering to achieve altitdue at a NAV_CMD_WAYPOINT */
|
||||
const bool enforce_exit_heading = _navigator->get_vstatus()->vehicle_type != vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
||||
const bool enforce_exit_heading = !_navigator_core.isRotaryWing()
|
||||
&&
|
||||
next_sp.valid &&
|
||||
curr_sp_new->type == position_setpoint_s::SETPOINT_TYPE_LOITER &&
|
||||
@ -379,12 +378,12 @@ MissionBlock::is_mission_item_reached()
|
||||
|
||||
float yaw_err = 0.0f;
|
||||
|
||||
if (dist_current_next > 1.2f * _navigator->get_loiter_radius()) {
|
||||
if (dist_current_next > 1.2f * _navigator_core.getLoiterRadiusMeter()) {
|
||||
// set required yaw from bearing to the next mission item
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(_navigator->get_global_position()->lat,
|
||||
_navigator->get_global_position()->lon,
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(_navigator_core.getLatRad(),
|
||||
_navigator_core.getLonRad(),
|
||||
next_sp.lat, next_sp.lon);
|
||||
const float cog = atan2f(_navigator->get_local_position()->vy, _navigator->get_local_position()->vx);
|
||||
const float cog = atan2f(_navigator_core.getVelEastMPS(), _navigator_core.getVelNorthMPS());
|
||||
yaw_err = wrap_pi(_mission_item.yaw - cog);
|
||||
|
||||
|
||||
@ -392,7 +391,7 @@ MissionBlock::is_mission_item_reached()
|
||||
}
|
||||
|
||||
|
||||
if (fabsf(yaw_err) < _navigator->get_yaw_threshold()) {
|
||||
if (fabsf(yaw_err) < _navigator_core.getWaypointHeadingAcceptanceRad()) {
|
||||
exit_heading_reached = true;
|
||||
}
|
||||
|
||||
@ -489,7 +488,7 @@ MissionBlock::issue_command(const mission_item_s &item)
|
||||
if (item.nav_cmd == NAV_CMD_DO_SET_ROI_LOCATION && item.altitude_is_relative) {
|
||||
vcmd.param5 = item.lat;
|
||||
vcmd.param6 = item.lon;
|
||||
vcmd.param7 = item.altitude + _navigator->get_home_position()->alt;
|
||||
vcmd.param7 = item.altitude + _navigator_core.getHomeAltAMSLMeter();
|
||||
|
||||
} else {
|
||||
vcmd.param5 = (double)item.params[4];
|
||||
@ -505,7 +504,7 @@ float
|
||||
MissionBlock::get_time_inside(const mission_item_s &item) const
|
||||
{
|
||||
if ((item.nav_cmd == NAV_CMD_WAYPOINT
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) ||
|
||||
&& _navigator_core.isRotaryWing()) ||
|
||||
item.nav_cmd == NAV_CMD_LOITER_TIME_LIMIT ||
|
||||
item.nav_cmd == NAV_CMD_DELAY) {
|
||||
|
||||
@ -553,10 +552,11 @@ MissionBlock::mission_item_to_position_setpoint(const mission_item_s &item, posi
|
||||
sp->lat = item.lat;
|
||||
sp->lon = item.lon;
|
||||
sp->alt = get_absolute_altitude_for_item(item);
|
||||
sp->alt_valid = true;
|
||||
sp->yaw = item.yaw;
|
||||
sp->yaw_valid = PX4_ISFINITE(item.yaw);
|
||||
sp->loiter_radius = (fabsf(item.loiter_radius) > NAV_EPSILON_POSITION) ? fabsf(item.loiter_radius) :
|
||||
_navigator->get_loiter_radius();
|
||||
_navigator_core.getLoiterRadiusMeter();
|
||||
sp->loiter_direction = (item.loiter_radius > 0) ? 1 : -1;
|
||||
|
||||
if (item.acceptance_radius > 0.0f && PX4_ISFINITE(item.acceptance_radius)) {
|
||||
@ -564,7 +564,7 @@ MissionBlock::mission_item_to_position_setpoint(const mission_item_s &item, posi
|
||||
sp->acceptance_radius = item.acceptance_radius;
|
||||
|
||||
} else {
|
||||
sp->acceptance_radius = _navigator->get_default_acceptance_radius();
|
||||
sp->acceptance_radius = _navigator->getCore().getDefaultHorAcceptanceRadiusMeter();
|
||||
}
|
||||
|
||||
sp->cruising_speed = _navigator->get_cruising_speed();
|
||||
@ -578,9 +578,8 @@ MissionBlock::mission_item_to_position_setpoint(const mission_item_s &item, posi
|
||||
case NAV_CMD_TAKEOFF:
|
||||
|
||||
// if already flying (armed and !landed) treat TAKEOFF like regular POSITION
|
||||
if ((_navigator->get_vstatus()->arming_state == vehicle_status_s::ARMING_STATE_ARMED)
|
||||
&& !_navigator->get_land_detected()->landed && !_navigator->get_land_detected()->maybe_landed) {
|
||||
|
||||
if ((_navigator_core.getArmingState() == vehicle_status_s::ARMING_STATE_ARMED)
|
||||
&& !_navigator_core.getLanded() && !_navigator_core.getMaybeLanded()) {
|
||||
sp->type = position_setpoint_s::SETPOINT_TYPE_POSITION;
|
||||
|
||||
} else {
|
||||
@ -601,12 +600,12 @@ MissionBlock::mission_item_to_position_setpoint(const mission_item_s &item, posi
|
||||
case NAV_CMD_LOITER_TO_ALT:
|
||||
|
||||
// initially use current altitude, and switch to mission item altitude once in loiter position
|
||||
if (_navigator->get_loiter_min_alt() > 0.f) { // ignore _param_loiter_min_alt if smaller than 0
|
||||
sp->alt = math::max(_navigator->get_global_position()->alt,
|
||||
_navigator->get_home_position()->alt + _navigator->get_loiter_min_alt());
|
||||
if (_navigator_core.getRelativeLoiterMinAltitudeMeter() > 0.f) { // ignore _param_loiter_min_alt if smaller than 0
|
||||
sp->alt = math::max(_navigator_core.getAltitudeAMSLMeters(),
|
||||
_navigator_core.getHomeAltAMSLMeter() + _navigator_core.getRelativeLoiterMinAltitudeMeter());
|
||||
|
||||
} else {
|
||||
sp->alt = _navigator->get_global_position()->alt;
|
||||
sp->alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
}
|
||||
|
||||
// FALLTHROUGH
|
||||
@ -630,7 +629,7 @@ MissionBlock::mission_item_to_position_setpoint(const mission_item_s &item, posi
|
||||
void
|
||||
MissionBlock::set_loiter_item(struct mission_item_s *item, float min_clearance)
|
||||
{
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
/* landed, don't takeoff, but switch to IDLE mode */
|
||||
item->nav_cmd = NAV_CMD_IDLE;
|
||||
|
||||
@ -647,19 +646,19 @@ MissionBlock::set_loiter_item(struct mission_item_s *item, float min_clearance)
|
||||
|
||||
} else {
|
||||
/* use current position and use return altitude as clearance */
|
||||
item->lat = _navigator->get_global_position()->lat;
|
||||
item->lon = _navigator->get_global_position()->lon;
|
||||
item->altitude = _navigator->get_global_position()->alt;
|
||||
item->lat = _navigator_core.getLatRad();
|
||||
item->lon = _navigator_core.getLonRad();
|
||||
item->altitude = _navigator_core.getAltitudeAMSLMeters();
|
||||
|
||||
if (min_clearance > 0.0f && item->altitude < _navigator->get_home_position()->alt + min_clearance) {
|
||||
item->altitude = _navigator->get_home_position()->alt + min_clearance;
|
||||
if (min_clearance > 0.0f && item->altitude < _navigator_core.getHomeAltAMSLMeter() + min_clearance) {
|
||||
item->altitude = _navigator_core.getHomeAltAMSLMeter() + min_clearance;
|
||||
}
|
||||
}
|
||||
|
||||
item->altitude_is_relative = false;
|
||||
item->yaw = NAN;
|
||||
item->loiter_radius = _navigator->get_loiter_radius();
|
||||
item->acceptance_radius = _navigator->get_acceptance_radius();
|
||||
item->loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
item->acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
item->time_inside = 0.0f;
|
||||
item->autocontinue = false;
|
||||
item->origin = ORIGIN_ONBOARD;
|
||||
@ -672,14 +671,14 @@ MissionBlock::set_takeoff_item(struct mission_item_s *item, float abs_altitude)
|
||||
item->nav_cmd = NAV_CMD_TAKEOFF;
|
||||
|
||||
/* use current position */
|
||||
item->lat = _navigator->get_global_position()->lat;
|
||||
item->lon = _navigator->get_global_position()->lon;
|
||||
item->yaw = _navigator->get_local_position()->heading;
|
||||
item->lat = _navigator_core.getLatRad();
|
||||
item->lon = _navigator_core.getLonRad();
|
||||
item->yaw = _navigator_core.getTrueHeadingRad();
|
||||
|
||||
item->altitude = abs_altitude;
|
||||
item->altitude_is_relative = false;
|
||||
|
||||
item->loiter_radius = _navigator->get_loiter_radius();
|
||||
item->loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
item->autocontinue = false;
|
||||
item->origin = ORIGIN_ONBOARD;
|
||||
}
|
||||
@ -688,7 +687,7 @@ void
|
||||
MissionBlock::set_land_item(struct mission_item_s *item, bool at_current_location)
|
||||
{
|
||||
/* VTOL transition to RW before landing */
|
||||
if (_navigator->force_vtol()) {
|
||||
if (_navigator_core.forceVTOL()) {
|
||||
|
||||
vehicle_command_s vcmd = {};
|
||||
vcmd.command = NAV_CMD_DO_VTOL_TRANSITION;
|
||||
@ -703,19 +702,19 @@ MissionBlock::set_land_item(struct mission_item_s *item, bool at_current_locatio
|
||||
if (at_current_location) {
|
||||
item->lat = (double)NAN; //descend at current position
|
||||
item->lon = (double)NAN; //descend at current position
|
||||
item->yaw = _navigator->get_local_position()->heading;
|
||||
item->yaw = _navigator_core.getTrueHeadingRad();
|
||||
|
||||
} else {
|
||||
/* use home position */
|
||||
item->lat = _navigator->get_home_position()->lat;
|
||||
item->lon = _navigator->get_home_position()->lon;
|
||||
item->yaw = _navigator->get_home_position()->yaw;
|
||||
item->lat = _navigator_core.getHomeLatRad();
|
||||
item->lon = _navigator_core.getHomeLonRad();
|
||||
item->yaw = _navigator_core.getHomeTrueHeadingRad();
|
||||
}
|
||||
|
||||
item->altitude = 0;
|
||||
item->altitude_is_relative = false;
|
||||
item->loiter_radius = _navigator->get_loiter_radius();
|
||||
item->acceptance_radius = _navigator->get_acceptance_radius();
|
||||
item->loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
item->acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
item->time_inside = 0.0f;
|
||||
item->autocontinue = true;
|
||||
item->origin = ORIGIN_ONBOARD;
|
||||
@ -725,13 +724,13 @@ void
|
||||
MissionBlock::set_idle_item(struct mission_item_s *item)
|
||||
{
|
||||
item->nav_cmd = NAV_CMD_IDLE;
|
||||
item->lat = _navigator->get_home_position()->lat;
|
||||
item->lon = _navigator->get_home_position()->lon;
|
||||
item->lat = _navigator_core.getHomeLatRad();
|
||||
item->lon = _navigator_core.getHomeLonRad();
|
||||
item->altitude_is_relative = false;
|
||||
item->altitude = _navigator->get_home_position()->alt;
|
||||
item->altitude = _navigator_core.getHomeAltAMSLMeter();
|
||||
item->yaw = NAN;
|
||||
item->loiter_radius = _navigator->get_loiter_radius();
|
||||
item->acceptance_radius = _navigator->get_acceptance_radius();
|
||||
item->loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
item->acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
item->time_inside = 0.0f;
|
||||
item->autocontinue = true;
|
||||
item->origin = ORIGIN_ONBOARD;
|
||||
@ -742,7 +741,7 @@ MissionBlock::set_vtol_transition_item(struct mission_item_s *item, const uint8_
|
||||
{
|
||||
item->nav_cmd = NAV_CMD_DO_VTOL_TRANSITION;
|
||||
item->params[0] = (float) new_mode;
|
||||
item->yaw = _navigator->get_local_position()->heading;
|
||||
item->yaw = _navigator_core.getTrueHeadingRad();
|
||||
item->autocontinue = true;
|
||||
}
|
||||
|
||||
@ -754,18 +753,18 @@ MissionBlock::mission_apply_limitation(mission_item_s &item)
|
||||
*/
|
||||
|
||||
/* do nothing if altitude max is negative */
|
||||
if (_navigator->get_land_detected()->alt_max > 0.0f) {
|
||||
if (_navigator_core.getLandDetectedAltMaxMeter() > 0.0f) {
|
||||
|
||||
/* absolute altitude */
|
||||
float altitude_abs = item.altitude_is_relative
|
||||
? item.altitude + _navigator->get_home_position()->alt
|
||||
? item.altitude + _navigator_core.getHomeAltAMSLMeter()
|
||||
: item.altitude;
|
||||
|
||||
/* limit altitude to maximum allowed altitude */
|
||||
if ((_navigator->get_land_detected()->alt_max + _navigator->get_home_position()->alt) < altitude_abs) {
|
||||
if ((_navigator_core.getLandDetectedAltMaxMeter() + _navigator_core.getHomeAltAMSLMeter()) < altitude_abs) {
|
||||
item.altitude = item.altitude_is_relative ?
|
||||
_navigator->get_land_detected()->alt_max :
|
||||
_navigator->get_land_detected()->alt_max + _navigator->get_home_position()->alt;
|
||||
_navigator_core.getLandDetectedAltMaxMeter() :
|
||||
_navigator_core.getLandDetectedAltMaxMeter() + _navigator_core.getHomeAltAMSLMeter();
|
||||
|
||||
}
|
||||
}
|
||||
@ -779,7 +778,7 @@ float
|
||||
MissionBlock::get_absolute_altitude_for_item(const mission_item_s &mission_item) const
|
||||
{
|
||||
if (mission_item.altitude_is_relative) {
|
||||
return mission_item.altitude + _navigator->get_home_position()->alt;
|
||||
return mission_item.altitude + _navigator_core.getHomeAltAMSLMeter();
|
||||
|
||||
} else {
|
||||
return mission_item.altitude;
|
||||
|
||||
@ -42,6 +42,7 @@
|
||||
|
||||
#include "navigator_mode.h"
|
||||
#include "navigation.h"
|
||||
#include "NavigatorCore.h"
|
||||
|
||||
#include <drivers/drv_hrt.h>
|
||||
#include <systemlib/mavlink_log.h>
|
||||
@ -61,7 +62,7 @@ public:
|
||||
/**
|
||||
* Constructor
|
||||
*/
|
||||
MissionBlock(Navigator *navigator);
|
||||
MissionBlock(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
virtual ~MissionBlock() = default;
|
||||
|
||||
MissionBlock(const MissionBlock &) = delete;
|
||||
@ -151,5 +152,7 @@ protected:
|
||||
|
||||
hrt_abstime _time_wp_reached{0};
|
||||
|
||||
NavigatorCore &_navigator_core;
|
||||
|
||||
uORB::Publication<actuator_controls_s> _actuator_pub{ORB_ID(actuator_controls_2)};
|
||||
};
|
||||
|
||||
@ -67,8 +67,8 @@ MissionFeasibilityChecker::checkMissionFeasible(const mission_s &mission,
|
||||
bool warned = false;
|
||||
|
||||
// first check if we have a valid position
|
||||
const bool home_valid = _navigator->home_position_valid();
|
||||
const bool home_alt_valid = _navigator->home_alt_valid();
|
||||
const bool home_valid = _navigator->getCore().isHomeValid();
|
||||
const bool home_alt_valid = _navigator->getCore().isHomeAltValid();
|
||||
|
||||
if (!home_alt_valid) {
|
||||
failed = true;
|
||||
@ -79,7 +79,7 @@ MissionFeasibilityChecker::checkMissionFeasible(const mission_s &mission,
|
||||
failed = failed || !checkDistanceToFirstWaypoint(mission, max_distance_to_1st_waypoint);
|
||||
}
|
||||
|
||||
const float home_alt = _navigator->get_home_position()->alt;
|
||||
const float home_alt = _navigator->getCore().getHomeAltAMSLMeter();
|
||||
|
||||
// check if all mission item commands are supported
|
||||
failed = failed || !checkMissionItemValidity(mission);
|
||||
@ -87,10 +87,10 @@ MissionFeasibilityChecker::checkMissionFeasible(const mission_s &mission,
|
||||
failed = failed || !checkGeofence(mission, home_alt, home_valid);
|
||||
failed = failed || !checkHomePositionAltitude(mission, home_alt, home_alt_valid, warned);
|
||||
|
||||
if (_navigator->get_vstatus()->is_vtol) {
|
||||
if (_navigator->getCore().isVTOL()) {
|
||||
failed = failed || !checkVTOL(mission, home_alt, false);
|
||||
|
||||
} else if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
} else if (_navigator->getCore().isRotaryWing()) {
|
||||
failed = failed || !checkRotarywing(mission, home_alt);
|
||||
|
||||
} else {
|
||||
@ -300,7 +300,7 @@ MissionFeasibilityChecker::checkMissionItemValidity(const mission_s &mission)
|
||||
}
|
||||
|
||||
// check if the mission starts with a land command while the vehicle is landed
|
||||
if ((i == 0) && missionitem.nav_cmd == NAV_CMD_LAND && _navigator->get_land_detected()->landed) {
|
||||
if ((i == 0) && missionitem.nav_cmd == NAV_CMD_LAND && _navigator->getCore().getLanded()) {
|
||||
|
||||
mavlink_log_critical(_navigator->get_mavlink_log_pub(), "Mission rejected: starts with landing");
|
||||
return false;
|
||||
@ -336,7 +336,7 @@ MissionFeasibilityChecker::checkTakeoff(const mission_s &mission, float home_alt
|
||||
: missionitem.altitude - home_alt;
|
||||
|
||||
// check if we should use default acceptance radius
|
||||
float acceptance_radius = _navigator->get_default_acceptance_radius();
|
||||
float acceptance_radius = _navigator->getCore().getDefaultHorAcceptanceRadiusMeter();
|
||||
|
||||
if (missionitem.acceptance_radius > NAV_EPSILON_POSITION) {
|
||||
acceptance_radius = missionitem.acceptance_radius;
|
||||
@ -408,7 +408,7 @@ MissionFeasibilityChecker::checkTakeoff(const mission_s &mission, float home_alt
|
||||
}
|
||||
}
|
||||
|
||||
if (_navigator->get_takeoff_required() && _navigator->get_land_detected()->landed) {
|
||||
if (_navigator->getCore().isTakeoffRequired() && _navigator->getCore().getLanded()) {
|
||||
// check for a takeoff waypoint, after the above conditions have been met
|
||||
// MIS_TAKEOFF_REQ param has to be set and the vehicle has to be landed - one can load a mission
|
||||
// while the vehicle is flying and it does not require a takeoff waypoint
|
||||
@ -653,7 +653,7 @@ MissionFeasibilityChecker::checkDistanceToFirstWaypoint(const mission_s &mission
|
||||
/* check distance from current position to item */
|
||||
float dist_to_1wp = get_distance_to_next_waypoint(
|
||||
mission_item.lat, mission_item.lon,
|
||||
_navigator->get_home_position()->lat, _navigator->get_home_position()->lon);
|
||||
_navigator->getCore().getHomeLatRad(), _navigator->getCore().getHomeLonRad());
|
||||
|
||||
if (dist_to_1wp < max_distance) {
|
||||
|
||||
|
||||
@ -122,6 +122,8 @@ public:
|
||||
|
||||
void publish_vehicle_cmd(vehicle_command_s *vcmd);
|
||||
|
||||
void params_update();
|
||||
|
||||
/**
|
||||
* Generate an artificial traffic indication
|
||||
*
|
||||
@ -165,39 +167,39 @@ public:
|
||||
const vehicle_roi_s &get_vroi() { return _vroi; }
|
||||
void reset_vroi() { _vroi = {}; }
|
||||
|
||||
bool home_alt_valid() { return (_home_pos.timestamp > 0 && _home_pos.valid_alt); }
|
||||
bool home_position_valid() { return (_home_pos.timestamp > 0 && _home_pos.valid_alt && _home_pos.valid_hpos && _home_pos.valid_lpos); }
|
||||
//bool home_alt_valid() { return (_home_pos.timestamp > 0 && _home_pos.valid_alt); }
|
||||
//bool _navigator_core.isHomeValid() { return (_home_pos.timestamp > 0 && _home_pos.valid_alt && _home_pos.valid_hpos && _home_pos.valid_lpos); }
|
||||
|
||||
Geofence &get_geofence() { return _geofence; }
|
||||
|
||||
bool get_can_loiter_at_sp() { return _can_loiter_at_sp; }
|
||||
float get_loiter_radius() { return _param_nav_loiter_rad.get(); }
|
||||
//float _navigator_core.getLoiterRadiusMeter() { return _param_nav_loiter_rad.get(); }
|
||||
|
||||
/**
|
||||
* Returns the default acceptance radius defined by the parameter
|
||||
*/
|
||||
float get_default_acceptance_radius();
|
||||
//float get_default_acceptance_radius();
|
||||
|
||||
/**
|
||||
* Get the acceptance radius
|
||||
*
|
||||
* @return the distance at which the next waypoint should be used
|
||||
*/
|
||||
float get_acceptance_radius();
|
||||
//float get_acceptance_radius();
|
||||
|
||||
/**
|
||||
* Get the default altitude acceptance radius (i.e. from parameters)
|
||||
*
|
||||
* @return the distance from the target altitude before considering the waypoint reached
|
||||
*/
|
||||
float get_default_altitude_acceptance_radius();
|
||||
//float get_default_altitude_acceptance_radius();
|
||||
|
||||
/**
|
||||
* Get the altitude acceptance radius
|
||||
*
|
||||
* @return the distance from the target altitude before considering the waypoint reached
|
||||
*/
|
||||
float get_altitude_acceptance_radius();
|
||||
//float get_altitude_acceptance_radius();
|
||||
|
||||
/**
|
||||
* Get the cruising speed
|
||||
@ -290,43 +292,21 @@ public:
|
||||
|
||||
void geofence_breach_check(bool &have_geofence_position_data);
|
||||
|
||||
// Param access
|
||||
float get_loiter_min_alt() const { return _param_mis_ltrmin_alt.get(); }
|
||||
float get_takeoff_min_alt() const { return _param_mis_takeoff_alt.get(); }
|
||||
bool get_takeoff_required() const { return _param_mis_takeoff_req.get(); }
|
||||
float get_yaw_timeout() const { return _param_mis_yaw_tmt.get(); }
|
||||
float get_yaw_threshold() const { return math::radians(_param_mis_yaw_err.get()); }
|
||||
|
||||
float get_vtol_back_trans_deceleration() const { return _param_back_trans_dec_mss; }
|
||||
float get_vtol_reverse_delay() const { return _param_reverse_delay; }
|
||||
|
||||
bool force_vtol();
|
||||
//bool force_vtol();
|
||||
|
||||
void acquire_gimbal_control();
|
||||
void release_gimbal_control();
|
||||
|
||||
NavigatorCore &getCore() { return _navigator_core; }
|
||||
|
||||
private:
|
||||
DEFINE_PARAMETERS(
|
||||
(ParamFloat<px4::params::NAV_LOITER_RAD>) _param_nav_loiter_rad, /**< loiter radius for fixedwing */
|
||||
(ParamFloat<px4::params::NAV_ACC_RAD>) _param_nav_acc_rad, /**< acceptance for takeoff */
|
||||
(ParamFloat<px4::params::NAV_FW_ALT_RAD>)
|
||||
_param_nav_fw_alt_rad, /**< acceptance radius for fixedwing altitude */
|
||||
(ParamFloat<px4::params::NAV_FW_ALTL_RAD>)
|
||||
_param_nav_fw_altl_rad, /**< acceptance radius for fixedwing altitude before landing*/
|
||||
(ParamFloat<px4::params::NAV_MC_ALT_RAD>)
|
||||
_param_nav_mc_alt_rad, /**< acceptance radius for multicopter altitude */
|
||||
(ParamInt<px4::params::NAV_FORCE_VT>) _param_nav_force_vt, /**< acceptance radius for multicopter altitude */
|
||||
(ParamInt<px4::params::NAV_TRAFF_AVOID>) _param_nav_traff_avoid, /**< avoiding other aircraft is enabled */
|
||||
(ParamFloat<px4::params::NAV_TRAFF_A_RADU>) _param_nav_traff_a_radu, /**< avoidance Distance Unmanned*/
|
||||
(ParamFloat<px4::params::NAV_TRAFF_A_RADM>) _param_nav_traff_a_radm, /**< avoidance Distance Manned*/
|
||||
|
||||
// non-navigator parameters
|
||||
// Mission (MIS_*)
|
||||
(ParamFloat<px4::params::MIS_LTRMIN_ALT>) _param_mis_ltrmin_alt,
|
||||
(ParamFloat<px4::params::MIS_TAKEOFF_ALT>) _param_mis_takeoff_alt,
|
||||
(ParamBool<px4::params::MIS_TAKEOFF_REQ>) _param_mis_takeoff_req,
|
||||
(ParamFloat<px4::params::MIS_YAW_TMT>) _param_mis_yaw_tmt,
|
||||
(ParamFloat<px4::params::MIS_YAW_ERR>) _param_mis_yaw_err
|
||||
(ParamFloat<px4::params::NAV_TRAFF_A_RADM>) _param_nav_traff_a_radm /**< avoidance Distance Manned*/
|
||||
)
|
||||
|
||||
int _local_pos_sub{-1};
|
||||
@ -385,6 +365,8 @@ private:
|
||||
bool _pos_sp_triplet_published_invalid_once{false}; /**< flags if position SP triplet has been published once to UORB */
|
||||
bool _mission_result_updated{false}; /**< flags if mission result has seen an update */
|
||||
|
||||
NavigatorCore _navigator_core;
|
||||
|
||||
NavigatorMode *_navigation_mode{nullptr}; /**< abstract pointer to current navigation mode class */
|
||||
Mission _mission; /**< class that handles the missions */
|
||||
Loiter _loiter; /**< class that handles loiter */
|
||||
@ -411,7 +393,7 @@ private:
|
||||
// if mission mode is inactive, this flag will be cleared after 2 seconds
|
||||
|
||||
// update subscriptions
|
||||
void params_update();
|
||||
|
||||
|
||||
/**
|
||||
* Publish a new position setpoint triplet for position controllers
|
||||
|
||||
@ -76,15 +76,16 @@ Navigator::Navigator() :
|
||||
_loop_perf(perf_alloc(PC_ELAPSED, "navigator")),
|
||||
_geofence(this),
|
||||
_gf_breach_avoidance(this),
|
||||
_mission(this),
|
||||
_loiter(this),
|
||||
_takeoff(this),
|
||||
_land(this),
|
||||
_precland(this),
|
||||
_rtl(this),
|
||||
_engineFailure(this),
|
||||
_gpsFailure(this),
|
||||
_follow_target(this)
|
||||
_navigator_core(),
|
||||
_mission(this, _navigator_core),
|
||||
_loiter(this, _navigator_core),
|
||||
_takeoff(this, _navigator_core),
|
||||
_land(this, _navigator_core),
|
||||
_precland(this, _navigator_core),
|
||||
_rtl(this, _navigator_core),
|
||||
_engineFailure(this, _navigator_core),
|
||||
_gpsFailure(this, _navigator_core),
|
||||
_follow_target(this, _navigator_core)
|
||||
{
|
||||
/* Create a list of our possible navigation types */
|
||||
_navigation_mode_array[0] = &_mission;
|
||||
@ -177,7 +178,9 @@ Navigator::run()
|
||||
perf_begin(_loop_perf);
|
||||
|
||||
orb_copy(ORB_ID(vehicle_local_position), _local_pos_sub, &_local_pos);
|
||||
_navigator_core.updateLocalPosition(_local_pos);
|
||||
orb_copy(ORB_ID(vehicle_status), _vehicle_status_sub, &_vstatus);
|
||||
_navigator_core.updateVehicleStatus(_vstatus);
|
||||
|
||||
if (fds[2].revents & POLLIN) {
|
||||
// copy mission to clear any update
|
||||
@ -197,6 +200,7 @@ Navigator::run()
|
||||
/* global position updated */
|
||||
if (_global_pos_sub.updated()) {
|
||||
_global_pos_sub.copy(&_global_pos);
|
||||
_navigator_core.updateGlobalPosition(_global_pos);
|
||||
|
||||
if (_geofence.getSource() == Geofence::GF_SOURCE_GLOBALPOS) {
|
||||
have_geofence_position_data = true;
|
||||
@ -214,8 +218,10 @@ Navigator::run()
|
||||
}
|
||||
|
||||
_land_detected_sub.update(&_land_detected);
|
||||
_navigator_core.updateLandedState(_land_detected);
|
||||
_position_controller_status_sub.update();
|
||||
_home_pos_sub.update(&_home_pos);
|
||||
_navigator_core.updateHomePosition(_home_pos);
|
||||
|
||||
while (_vehicle_command_sub.updated()) {
|
||||
const unsigned last_generation = _vehicle_command_sub.get_last_generation();
|
||||
@ -254,7 +260,7 @@ Navigator::run()
|
||||
}
|
||||
|
||||
reposition_valid = _geofence.check(test_reposition_validity, _gps_pos, _home_pos,
|
||||
home_position_valid());
|
||||
_navigator_core.isHomeValid());
|
||||
}
|
||||
}
|
||||
|
||||
@ -268,7 +274,7 @@ Navigator::run()
|
||||
rep->previous.lon = get_global_position()->lon;
|
||||
rep->previous.alt = get_global_position()->alt;
|
||||
|
||||
rep->current.loiter_radius = get_loiter_radius();
|
||||
rep->current.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
rep->current.loiter_direction = 1;
|
||||
rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
|
||||
|
||||
@ -281,7 +287,7 @@ Navigator::run()
|
||||
}
|
||||
|
||||
rep->current.cruising_throttle = get_cruising_throttle();
|
||||
rep->current.acceptance_radius = get_acceptance_radius();
|
||||
rep->current.acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
|
||||
// Go on and check which changes had been requested
|
||||
if (PX4_ISFINITE(cmd.param4)) {
|
||||
@ -351,11 +357,11 @@ Navigator::run()
|
||||
rep->previous.lon = get_global_position()->lon;
|
||||
rep->previous.alt = get_global_position()->alt;
|
||||
|
||||
rep->current.loiter_radius = get_loiter_radius();
|
||||
rep->current.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
rep->current.loiter_direction = 1;
|
||||
rep->current.type = position_setpoint_s::SETPOINT_TYPE_TAKEOFF;
|
||||
|
||||
if (home_position_valid()) {
|
||||
if (_navigator_core.isHomeValid()) {
|
||||
rep->current.yaw = cmd.param4;
|
||||
|
||||
rep->previous.valid = true;
|
||||
@ -721,7 +727,7 @@ void Navigator::geofence_breach_check(bool &have_geofence_position_data)
|
||||
vertical_test_point_distance = _gf_breach_avoidance.computeVerticalBrakingDistanceMultirotor();
|
||||
|
||||
} else {
|
||||
test_point_distance = 2.0f * get_loiter_radius();
|
||||
test_point_distance = 2.0f * _navigator_core.getLoiterRadiusMeter();
|
||||
vertical_test_point_distance = 5.0f;
|
||||
|
||||
if (hrt_absolute_time() - pos_ctrl_status.timestamp < 100000 && PX4_ISFINITE(pos_ctrl_status.nav_bearing)) {
|
||||
@ -739,7 +745,7 @@ void Navigator::geofence_breach_check(bool &have_geofence_position_data)
|
||||
_gf_breach_avoidance.setMaxHorDistHome(_geofence.getMaxHorDistanceHome());
|
||||
_gf_breach_avoidance.setMaxVerDistHome(_geofence.getMaxVerDistanceHome());
|
||||
|
||||
if (home_position_valid()) {
|
||||
if (_navigator_core.isHomeValid()) {
|
||||
_gf_breach_avoidance.setHomePosition(_home_pos.lat, _home_pos.lon, _home_pos.alt);
|
||||
}
|
||||
|
||||
@ -802,12 +808,12 @@ void Navigator::geofence_breach_check(bool &have_geofence_position_data)
|
||||
rep->current.lon = lointer_center_lat_lon(1);
|
||||
rep->current.alt = loiter_altitude_amsl;
|
||||
rep->current.valid = true;
|
||||
rep->current.loiter_radius = get_loiter_radius();
|
||||
rep->current.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
rep->current.alt_valid = true;
|
||||
rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
|
||||
rep->current.loiter_direction = 1;
|
||||
rep->current.cruising_throttle = get_cruising_throttle();
|
||||
rep->current.acceptance_radius = get_acceptance_radius();
|
||||
rep->current.acceptance_radius = _navigator_core.getHorAcceptanceRadiusMeter();
|
||||
rep->current.cruising_speed = get_cruising_speed();
|
||||
|
||||
}
|
||||
@ -872,36 +878,13 @@ Navigator::publish_position_setpoint_triplet()
|
||||
_pos_sp_triplet_updated = false;
|
||||
}
|
||||
|
||||
float
|
||||
Navigator::get_default_acceptance_radius()
|
||||
{
|
||||
return _param_nav_acc_rad.get();
|
||||
}
|
||||
// float
|
||||
// Navigator::get_default_acceptance_radius()
|
||||
// {
|
||||
// return _navigator_core.getDefaultHorAcceptanceRadiusMeter();
|
||||
// }
|
||||
|
||||
float
|
||||
Navigator::get_default_altitude_acceptance_radius()
|
||||
{
|
||||
if (get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING) {
|
||||
return _param_nav_fw_alt_rad.get();
|
||||
|
||||
} else if (get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROVER) {
|
||||
return INFINITY;
|
||||
|
||||
} else {
|
||||
float alt_acceptance_radius = _param_nav_mc_alt_rad.get();
|
||||
|
||||
const position_controller_status_s &pos_ctrl_status = _position_controller_status_sub.get();
|
||||
|
||||
if ((pos_ctrl_status.timestamp > _pos_sp_triplet.timestamp)
|
||||
&& pos_ctrl_status.altitude_acceptance > alt_acceptance_radius) {
|
||||
alt_acceptance_radius = pos_ctrl_status.altitude_acceptance;
|
||||
}
|
||||
|
||||
return alt_acceptance_radius;
|
||||
}
|
||||
}
|
||||
|
||||
float
|
||||
/* float
|
||||
Navigator::get_altitude_acceptance_radius()
|
||||
{
|
||||
if (get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING) {
|
||||
@ -914,7 +897,7 @@ Navigator::get_altitude_acceptance_radius()
|
||||
}
|
||||
|
||||
return get_default_altitude_acceptance_radius();
|
||||
}
|
||||
} */
|
||||
|
||||
float
|
||||
Navigator::get_cruising_speed()
|
||||
@ -973,8 +956,8 @@ Navigator::reset_position_setpoint(position_setpoint_s &sp)
|
||||
sp.timestamp = hrt_absolute_time();
|
||||
sp.lat = static_cast<double>(NAN);
|
||||
sp.lon = static_cast<double>(NAN);;
|
||||
sp.loiter_radius = get_loiter_radius();
|
||||
sp.acceptance_radius = get_default_acceptance_radius();
|
||||
sp.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
sp.acceptance_radius = _navigator_core.getDefaultHorAcceptanceRadiusMeter();
|
||||
sp.cruising_speed = get_cruising_speed();
|
||||
sp.cruising_throttle = get_cruising_throttle();
|
||||
sp.valid = false;
|
||||
@ -994,7 +977,7 @@ Navigator::get_cruising_throttle()
|
||||
}
|
||||
}
|
||||
|
||||
float
|
||||
/* float
|
||||
Navigator::get_acceptance_radius()
|
||||
{
|
||||
float acceptance_radius = get_default_acceptance_radius(); // the value specified in the parameter NAV_ACC_RAD
|
||||
@ -1008,7 +991,7 @@ Navigator::get_acceptance_radius()
|
||||
}
|
||||
|
||||
return acceptance_radius;
|
||||
}
|
||||
} */
|
||||
|
||||
float
|
||||
Navigator::get_yaw_acceptance(float mission_item_yaw)
|
||||
@ -1270,13 +1253,13 @@ Navigator::abort_landing()
|
||||
return should_abort;
|
||||
}
|
||||
|
||||
bool
|
||||
/* bool
|
||||
Navigator::force_vtol()
|
||||
{
|
||||
return _vstatus.is_vtol &&
|
||||
(_vstatus.vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING || _vstatus.in_transition_to_fw)
|
||||
&& _param_nav_force_vt.get();
|
||||
}
|
||||
} */
|
||||
|
||||
int Navigator::custom_command(int argc, char *argv[])
|
||||
{
|
||||
|
||||
@ -59,8 +59,8 @@
|
||||
|
||||
#define STATE_TIMEOUT 10000000 // [us] Maximum time to spend in any state
|
||||
|
||||
PrecLand::PrecLand(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
PrecLand::PrecLand(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, _navigator_core),
|
||||
ModuleParams(navigator)
|
||||
{
|
||||
_handle_param_acceleration_hor = param_find("MPC_ACC_HOR");
|
||||
@ -90,9 +90,9 @@ PrecLand::on_activation()
|
||||
// Check that the current position setpoint is valid, otherwise land at current position
|
||||
if (!pos_sp_triplet->current.valid) {
|
||||
PX4_WARN("Resetting landing position to current position");
|
||||
pos_sp_triplet->current.lat = _navigator->get_global_position()->lat;
|
||||
pos_sp_triplet->current.lon = _navigator->get_global_position()->lon;
|
||||
pos_sp_triplet->current.alt = _navigator->get_global_position()->alt;
|
||||
pos_sp_triplet->current.lat = _navigator_core.getLatRad();
|
||||
pos_sp_triplet->current.lon = _navigator_core.getLonRad();
|
||||
pos_sp_triplet->current.alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
pos_sp_triplet->current.valid = true;
|
||||
pos_sp_triplet->current.timestamp = hrt_absolute_time();
|
||||
}
|
||||
@ -121,7 +121,7 @@ PrecLand::on_active()
|
||||
}
|
||||
|
||||
// stop if we are landed
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
switch_to_state_done();
|
||||
}
|
||||
|
||||
@ -198,10 +198,10 @@ PrecLand::run_state_start()
|
||||
|
||||
position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
float dist = get_distance_to_next_waypoint(pos_sp_triplet->current.lat, pos_sp_triplet->current.lon,
|
||||
_navigator->get_global_position()->lat, _navigator->get_global_position()->lon);
|
||||
_navigator_core.getLatRad(), _navigator_core.getLonRad());
|
||||
|
||||
// check if we've reached the start point
|
||||
if (dist < _navigator->get_acceptance_radius()) {
|
||||
if (dist < _navigator_core.getAcceptanceRadiusMeter()) {
|
||||
if (!_point_reached_time) {
|
||||
_point_reached_time = hrt_absolute_time();
|
||||
}
|
||||
@ -235,9 +235,9 @@ PrecLand::run_state_horizontal_approach()
|
||||
PX4_WARN("Lost landing target while landing (horizontal approach).");
|
||||
|
||||
// Stay at current position for searching for the landing target
|
||||
pos_sp_triplet->current.lat = _navigator->get_global_position()->lat;
|
||||
pos_sp_triplet->current.lon = _navigator->get_global_position()->lon;
|
||||
pos_sp_triplet->current.alt = _navigator->get_global_position()->alt;
|
||||
pos_sp_triplet->current.lat = _navigator_core.getLatRad();
|
||||
pos_sp_triplet->current.lon = _navigator_core.getLonRad();
|
||||
pos_sp_triplet->current.alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
|
||||
if (!switch_to_state_start()) {
|
||||
if (!switch_to_state_fallback()) {
|
||||
@ -300,9 +300,9 @@ PrecLand::run_state_descend_above_target()
|
||||
PX4_WARN("Lost landing target while landing (descending).");
|
||||
|
||||
// Stay at current position for searching for the target
|
||||
pos_sp_triplet->current.lat = _navigator->get_global_position()->lat;
|
||||
pos_sp_triplet->current.lon = _navigator->get_global_position()->lon;
|
||||
pos_sp_triplet->current.alt = _navigator->get_global_position()->alt;
|
||||
pos_sp_triplet->current.lat = _navigator_core.getLatRad();
|
||||
pos_sp_triplet->current.lon = _navigator_core.getLonRad();
|
||||
pos_sp_triplet->current.alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
|
||||
if (!switch_to_state_start()) {
|
||||
if (!switch_to_state_fallback()) {
|
||||
@ -341,7 +341,7 @@ PrecLand::run_state_search()
|
||||
// target just became visible. Stop climbing, but give it some margin so we don't stop too apruptly
|
||||
_target_acquired_time = hrt_absolute_time();
|
||||
position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
float new_alt = _navigator->get_global_position()->alt + 1.0f;
|
||||
float new_alt = _navigator_core.getAltitudeAMSLMeters() + 1.0f;
|
||||
pos_sp_triplet->current.alt = new_alt < pos_sp_triplet->current.alt ? new_alt : pos_sp_triplet->current.alt;
|
||||
_navigator->set_position_setpoint_triplet_updated();
|
||||
}
|
||||
@ -395,7 +395,7 @@ bool
|
||||
PrecLand::switch_to_state_horizontal_approach()
|
||||
{
|
||||
if (check_state_conditions(PrecLandState::HorizontalApproach)) {
|
||||
_approach_alt = _navigator->get_global_position()->alt;
|
||||
_approach_alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
|
||||
_point_reached_time = 0;
|
||||
|
||||
@ -454,9 +454,9 @@ PrecLand::switch_to_state_fallback()
|
||||
{
|
||||
PX4_WARN("Falling back to normal land.");
|
||||
position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
pos_sp_triplet->current.lat = _navigator->get_global_position()->lat;
|
||||
pos_sp_triplet->current.lon = _navigator->get_global_position()->lon;
|
||||
pos_sp_triplet->current.alt = _navigator->get_global_position()->alt;
|
||||
pos_sp_triplet->current.lat = _navigator_core.getLatRad();
|
||||
pos_sp_triplet->current.lon = _navigator_core.getLonRad();
|
||||
pos_sp_triplet->current.alt = _navigator_core.getAltitudeAMSLMeters();
|
||||
pos_sp_triplet->current.type = position_setpoint_s::SETPOINT_TYPE_LAND;
|
||||
_navigator->set_position_setpoint_triplet_updated();
|
||||
|
||||
@ -557,8 +557,8 @@ void PrecLand::slewrate(float &sp_x, float &sp_y)
|
||||
// set a best guess for previous setpoints for smooth transition
|
||||
map_projection_project(&_map_ref, _navigator->get_position_setpoint_triplet()->current.lat,
|
||||
_navigator->get_position_setpoint_triplet()->current.lon, &_sp_pev(0), &_sp_pev(1));
|
||||
_sp_pev_prev(0) = _sp_pev(0) - _navigator->get_local_position()->vx * dt;
|
||||
_sp_pev_prev(1) = _sp_pev(1) - _navigator->get_local_position()->vy * dt;
|
||||
_sp_pev_prev(0) = _sp_pev(0) - _navigator_core.getVelNorthMPS() * dt;
|
||||
_sp_pev_prev(1) = _sp_pev(1) - _navigator_core.getVelEastMPS() * dt;
|
||||
}
|
||||
|
||||
_last_slewrate_time = now;
|
||||
|
||||
@ -67,7 +67,7 @@ enum class PrecLandMode {
|
||||
class PrecLand : public MissionBlock, public ModuleParams
|
||||
{
|
||||
public:
|
||||
PrecLand(Navigator *navigator);
|
||||
PrecLand(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~PrecLand() override = default;
|
||||
|
||||
void on_activation() override;
|
||||
|
||||
@ -52,8 +52,8 @@ static constexpr float DELAY_SIGMA = 0.01f;
|
||||
using namespace time_literals;
|
||||
using namespace math;
|
||||
|
||||
RTL::RTL(Navigator *navigator) :
|
||||
MissionBlock(navigator),
|
||||
RTL::RTL(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core),
|
||||
ModuleParams(navigator)
|
||||
{
|
||||
}
|
||||
@ -80,14 +80,14 @@ void RTL::find_RTL_destination()
|
||||
return;
|
||||
}
|
||||
|
||||
if (!_navigator->home_position_valid()) {
|
||||
if (!_navigator_core.isHomeValid()) {
|
||||
return;
|
||||
}
|
||||
|
||||
_destination_check_time = hrt_absolute_time();
|
||||
|
||||
// get home position:
|
||||
home_position_s &home_landing_position = *_navigator->get_home_position();
|
||||
home_position_s &home_landing_position = _navigator_core.getHomePosition();
|
||||
|
||||
// get global position
|
||||
const vehicle_global_position_s &global_position = *_navigator->get_global_position();
|
||||
@ -110,8 +110,8 @@ void RTL::find_RTL_destination()
|
||||
|
||||
_destination.type = RTL_DESTINATION_HOME;
|
||||
|
||||
const bool vtol_in_rw_mode = _navigator->get_vstatus()->is_vtol
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
|
||||
const bool vtol_in_rw_mode = _navigator_core.isVTOL()
|
||||
&& _navigator_core.isRotaryWing();
|
||||
|
||||
|
||||
// consider the mission landing if not RTL_HOME type set
|
||||
@ -237,8 +237,8 @@ void RTL::find_RTL_destination()
|
||||
void RTL::on_activation()
|
||||
{
|
||||
|
||||
_deny_mission_landing = _navigator->get_vstatus()->is_vtol
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
|
||||
_deny_mission_landing = _navigator_core.isVTOL()
|
||||
&& _navigator_core.isRotaryWing();
|
||||
|
||||
// output the correct message, depending on where the RTL destination is
|
||||
switch (_destination.type) {
|
||||
@ -259,16 +259,15 @@ void RTL::on_activation()
|
||||
|
||||
_rtl_loiter_rad = _param_rtl_loiter_rad.get();
|
||||
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
if (_navigator_core.isRotaryWing()) {
|
||||
_rtl_alt = calculate_return_alt_from_cone_half_angle((float)_param_rtl_cone_half_angle_deg.get());
|
||||
|
||||
} else {
|
||||
_rtl_alt = max(global_position.alt, max(_destination.alt,
|
||||
_navigator->get_home_position()->alt + _param_rtl_return_alt.get()));
|
||||
_navigator_core.getHomeAltAMSLMeter() + _param_rtl_return_alt.get()));
|
||||
}
|
||||
|
||||
|
||||
if (_navigator->get_land_detected()->landed) {
|
||||
if (_navigator_core.getLanded()) {
|
||||
// For safety reasons don't go into RTL if landed.
|
||||
_rtl_state = RTL_STATE_LANDED;
|
||||
|
||||
@ -343,7 +342,7 @@ void RTL::set_rtl_item()
|
||||
|
||||
// do not use LOITER_TO_ALT for rotary wing mode as it would then always climb to at least MIS_LTRMIN_ALT,
|
||||
// even if current climb altitude is below (e.g. RTL immediately after take off)
|
||||
if (_navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
if (_navigator_core.isRotaryWing()) {
|
||||
_mission_item.nav_cmd = NAV_CMD_WAYPOINT;
|
||||
|
||||
} else {
|
||||
@ -354,8 +353,8 @@ void RTL::set_rtl_item()
|
||||
_mission_item.lon = gpos.lon;
|
||||
_mission_item.altitude = _rtl_alt;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.yaw = _navigator->get_local_position()->heading;
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.yaw = _navigator_core.getTrueHeadingRad();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = 0.0f;
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -383,7 +382,7 @@ void RTL::set_rtl_item()
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(gpos.lat, gpos.lon, _destination.lat, _destination.lon);
|
||||
}
|
||||
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = 0.0f;
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -405,18 +404,18 @@ void RTL::set_rtl_item()
|
||||
// Except for vtol which might be still off here and should point towards this location.
|
||||
const float d_current = get_distance_to_next_waypoint(gpos.lat, gpos.lon, _mission_item.lat, _mission_item.lon);
|
||||
|
||||
if (_navigator->get_vstatus()->is_vtol && (d_current > _navigator->get_acceptance_radius())) {
|
||||
if (_navigator_core.isVTOL() && (d_current > _navigator_core.getAcceptanceRadiusMeter())) {
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(gpos.lat, gpos.lon, _mission_item.lat, _mission_item.lon);
|
||||
|
||||
} else {
|
||||
_mission_item.yaw = _destination.yaw;
|
||||
}
|
||||
|
||||
if (_navigator->get_vstatus()->is_vtol) {
|
||||
if (_navigator->getCore().isVTOL()) {
|
||||
_mission_item.loiter_radius = _rtl_loiter_rad;
|
||||
}
|
||||
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = 0.0f;
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -438,8 +437,8 @@ void RTL::set_rtl_item()
|
||||
_mission_item.altitude = loiter_altitude;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.yaw = _destination.yaw;
|
||||
_mission_item.loiter_radius = _navigator->get_loiter_radius();
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.loiter_radius = _navigator_core.getLoiterRadiusMeter();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = max(_param_rtl_land_delay.get(), 0.0f);
|
||||
_mission_item.autocontinue = autoland;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -467,7 +466,7 @@ void RTL::set_rtl_item()
|
||||
_mission_item.altitude = loiter_altitude;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(gpos.lat, gpos.lon, _mission_item.lat, _mission_item.lon);
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = 0.0f;
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -489,7 +488,7 @@ void RTL::set_rtl_item()
|
||||
_mission_item.altitude = loiter_altitude;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.yaw = get_bearing_to_next_waypoint(gpos.lat, gpos.lon, _mission_item.lat, _mission_item.lon);
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
break;
|
||||
}
|
||||
@ -502,7 +501,7 @@ void RTL::set_rtl_item()
|
||||
_mission_item.yaw = _destination.yaw;
|
||||
_mission_item.altitude = _destination.alt;
|
||||
_mission_item.altitude_is_relative = false;
|
||||
_mission_item.acceptance_radius = _navigator->get_acceptance_radius();
|
||||
_mission_item.acceptance_radius = _navigator_core.getAcceptanceRadiusMeter();
|
||||
_mission_item.time_inside = 0.0f;
|
||||
_mission_item.autocontinue = true;
|
||||
_mission_item.origin = ORIGIN_ONBOARD;
|
||||
@ -552,8 +551,8 @@ void RTL::advance_rtl()
|
||||
const bool descend_and_loiter = _param_rtl_land_delay.get() < -DELAY_SIGMA || _param_rtl_land_delay.get() > DELAY_SIGMA;
|
||||
|
||||
// vehicle is a vtol and currently in fixed wing mode
|
||||
const bool vtol_in_fw_mode = _navigator->get_vstatus()->is_vtol
|
||||
&& _navigator->get_vstatus()->vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING;
|
||||
const bool vtol_in_fw_mode = _navigator_core.isVTOL()
|
||||
&& _navigator_core.isFixedWing();
|
||||
|
||||
switch (_rtl_state) {
|
||||
case RTL_STATE_CLIMB:
|
||||
@ -635,11 +634,11 @@ float RTL::calculate_return_alt_from_cone_half_angle(float cone_half_angle_deg)
|
||||
// We choose the minimum height to be two times the distance from the land position in order to
|
||||
// avoid the vehicle touching the ground while still moving horizontally.
|
||||
const float return_altitude_min_outside_acceptance_rad_amsl = _destination.alt + 2.0f *
|
||||
_navigator->get_acceptance_radius();
|
||||
_navigator_core.getAcceptanceRadiusMeter();
|
||||
|
||||
float return_altitude_amsl = _destination.alt + _param_rtl_return_alt.get();
|
||||
|
||||
if (destination_dist <= _navigator->get_acceptance_radius()) {
|
||||
if (destination_dist <= _navigator_core.getAcceptanceRadiusMeter()) {
|
||||
return_altitude_amsl = _destination.alt + 2.0f * destination_dist;
|
||||
|
||||
} else {
|
||||
@ -663,7 +662,7 @@ float RTL::calculate_return_alt_from_cone_half_angle(float cone_half_angle_deg)
|
||||
|
||||
void RTL::get_rtl_xy_z_speed(float &xy, float &z)
|
||||
{
|
||||
uint8_t vehicle_type = _navigator->get_vstatus()->vehicle_type;
|
||||
uint8_t vehicle_type = _navigator_core.getVehicleType();
|
||||
// Caution: here be dragons!
|
||||
// Use C API to allow this code to be compiled with builds that don't have FW/MC/Rover
|
||||
|
||||
|
||||
@ -72,7 +72,7 @@ public:
|
||||
RTL_DESTINATION_SAFE_POINT,
|
||||
};
|
||||
|
||||
RTL(Navigator *navigator);
|
||||
RTL(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
|
||||
~RTL() = default;
|
||||
|
||||
|
||||
@ -41,8 +41,10 @@
|
||||
#include "takeoff.h"
|
||||
#include "navigator.h"
|
||||
|
||||
Takeoff::Takeoff(Navigator *navigator) :
|
||||
MissionBlock(navigator)
|
||||
using matrix::wrap_pi;
|
||||
|
||||
Takeoff::Takeoff(Navigator *navigator, NavigatorCore &navigator_core) :
|
||||
MissionBlock(navigator, navigator_core)
|
||||
{
|
||||
}
|
||||
|
||||
@ -64,7 +66,6 @@ Takeoff::on_active()
|
||||
} else if (is_mission_item_reached() && !_navigator->get_mission_result()->finished) {
|
||||
_navigator->get_mission_result()->finished = true;
|
||||
_navigator->set_mission_result_updated();
|
||||
|
||||
// set loiter item so position controllers stop doing takeoff logic
|
||||
set_loiter_item(&_mission_item);
|
||||
struct position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
|
||||
@ -83,22 +84,22 @@ Takeoff::set_takeoff_position()
|
||||
|
||||
float min_abs_altitude;
|
||||
|
||||
if (_navigator->home_position_valid()) { //only use home position if it is valid
|
||||
min_abs_altitude = _navigator->get_global_position()->alt + _navigator->get_takeoff_min_alt();
|
||||
if (_navigator_core.isHomeValid()) { //only use home position if it is valid
|
||||
min_abs_altitude = _navigator_core.getAltitudeAMSLMeters() + _navigator_core.getRelativeTakeoffMinAltitudeMeter();
|
||||
|
||||
} else { //e.g. flow
|
||||
min_abs_altitude = _navigator->get_takeoff_min_alt();
|
||||
min_abs_altitude = _navigator_core.getRelativeTakeoffMinAltitudeMeter();
|
||||
}
|
||||
|
||||
// Use altitude if it has been set. If home position is invalid use min_abs_altitude
|
||||
if (rep->current.valid && PX4_ISFINITE(rep->current.alt) && _navigator->home_position_valid()) {
|
||||
if (rep->current.valid && PX4_ISFINITE(rep->current.alt) && _navigator_core.isHomeValid()) {
|
||||
abs_altitude = rep->current.alt;
|
||||
|
||||
// If the altitude suggestion is lower than home + minimum clearance, raise it and complain.
|
||||
if (abs_altitude < min_abs_altitude) {
|
||||
if (abs_altitude < min_abs_altitude - 0.1f) { // don't complain if difference is smaller than 10cm
|
||||
mavlink_log_critical(_navigator->get_mavlink_log_pub(),
|
||||
"Using minimum takeoff altitude: %.2f m", (double)_navigator->get_takeoff_min_alt());
|
||||
"Using minimum takeoff altitude: %.2f m", (double)_navigator_core.getRelativeTakeoffMinAltitudeMeter());
|
||||
}
|
||||
|
||||
abs_altitude = min_abs_altitude;
|
||||
@ -108,13 +109,13 @@ Takeoff::set_takeoff_position()
|
||||
// Use home + minimum clearance but only notify.
|
||||
abs_altitude = min_abs_altitude;
|
||||
mavlink_log_info(_navigator->get_mavlink_log_pub(),
|
||||
"Using minimum takeoff altitude: %.2f m", (double)_navigator->get_takeoff_min_alt());
|
||||
"Using minimum takeoff altitude: %.2f m", (double)_navigator_core.getRelativeTakeoffMinAltitudeMeter());
|
||||
}
|
||||
|
||||
|
||||
if (abs_altitude < _navigator->get_global_position()->alt) {
|
||||
if (abs_altitude < _navigator_core.getAltitudeAMSLMeters()) {
|
||||
// If the suggestion is lower than our current alt, let's not go down.
|
||||
abs_altitude = _navigator->get_global_position()->alt;
|
||||
abs_altitude = _navigator_core.getAltitudeAMSLMeters();
|
||||
mavlink_log_critical(_navigator->get_mavlink_log_pub(), "Already higher than takeoff altitude");
|
||||
}
|
||||
|
||||
|
||||
@ -46,7 +46,7 @@
|
||||
class Takeoff : public MissionBlock
|
||||
{
|
||||
public:
|
||||
Takeoff(Navigator *navigator);
|
||||
Takeoff(Navigator *navigator, NavigatorCore &navigator_core);
|
||||
~Takeoff() = default;
|
||||
|
||||
void on_activation() override;
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user