navigator: wrote unit tests for Takeoff navigation mode

Signed-off-by: RomanBapst <bapstroman@gmail.com>
This commit is contained in:
RomanBapst 2021-05-12 18:29:54 +03:00
parent ad0482155e
commit 18a5bb32bc
31 changed files with 792 additions and 393 deletions

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@ -51,6 +51,7 @@ px4_add_module(
enginefailure.cpp
gpsfailure.cpp
follow_target.cpp
NavigatorCore.cpp
DEPENDS
git_ecl
ecl_geo
@ -59,4 +60,5 @@ px4_add_module(
motion_planning
)
px4_add_functional_gtest(SRC RangeRTLTest.cpp LINKLIBS modules__navigator modules__dataman)
px4_add_functional_gtest(SRC RangeRTLTest.cpp LINKLIBS modules__navigator modules__dataman)
px4_add_functional_gtest(SRC NavigatorModeTakeoffTest.cpp LINKLIBS modules__navigator modules__dataman)

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@ -0,0 +1,17 @@
#pragma once
#define MODULE_NAME "navigator"
#include <navigator/navigator.h>
class FakeNavigator : public Navigator
{
public:
FakeNavigator() :
Navigator() {};
virtual ~FakeNavigator() {};
private:
};

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@ -34,7 +34,7 @@
#include <gtest/gtest.h>
#include "geofence_breach_avoidance.h"
#include "fake_geofence.hpp"
#include "dataman_mocks.hpp"
#include <dataman/dataman_mocks.hpp>
#include <parameters/param.h>
using namespace matrix;

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@ -0,0 +1,131 @@
/***************************************************************************
*
* Copyright (c) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file NavigatorCore.cpp
*
*/
#include "NavigatorCore.h"
#include <px4_platform_common/defines.h>
NavigatorCore::NavigatorCore() :
ModuleParams(nullptr)
{
}
NavigatorCore::~NavigatorCore()
{
}
bool NavigatorCore::forceVTOL()
{
return _status.is_vtol && (isRotaryWing() || _status.in_transition_to_fw) && _param_nav_force_vt.get();
}
float NavigatorCore::getHorAcceptanceRadiusMeter()
{
if (isRotaryWing()) {
return getDefaultHorAcceptanceRadiusMeter();
} else {
return math::max(_pos_ctrl_status.acceptance_radius, getDefaultHorAcceptanceRadiusMeter());
}
}
float NavigatorCore::getAltAcceptanceRadMeter()
{
if (isFixedWing()) {
const position_setpoint_s &next_sp = getCurrentTriplet().next;
if (next_sp.type == position_setpoint_s::SETPOINT_TYPE_LAND && next_sp.valid) {
// Use separate (tighter) altitude acceptance for clean altitude starting point before landing
return getFixedWingLandingAltAcceptanceRadius();
}
}
return getDefaultAltAcceptanceRadiusMeter();
}
float NavigatorCore::getDefaultAltAcceptanceRadiusMeter()
{
if (isFixedWing()) {
return getFixedWingAltAcceptanceRadiusMeter();
} else if (isRover()) {
return INFINITY;
} else {
float alt_acceptance_radius = getMulticopterAltAcceptanceRadiusMeter();
if ((_pos_ctrl_status.timestamp > getCurrentTriplet().timestamp)
&& _pos_ctrl_status.altitude_acceptance > alt_acceptance_radius) {
alt_acceptance_radius = _pos_ctrl_status.altitude_acceptance;
}
return alt_acceptance_radius;
}
}
float NavigatorCore::getAcceptanceRadiusMeter()
{
float acceptance_radius = _param_nav_acc_rad.get();
// for fixed-wing and rover, return the max of NAV_ACC_RAD and the controller acceptance radius (e.g. L1 distance)
if (!isRotaryWing() && PX4_ISFINITE(_pos_ctrl_status.acceptance_radius) && _pos_ctrl_status.timestamp != 0) {
acceptance_radius = math::max(acceptance_radius, _pos_ctrl_status.acceptance_radius);
}
return acceptance_radius;
}
float NavigatorCore::getAltAcceptanceRadiusMeter()
{
if (isFixedWing()) {
const position_setpoint_s &next_sp = _triplet.next;
if (next_sp.type == position_setpoint_s::SETPOINT_TYPE_LAND && next_sp.valid) {
// Use separate (tighter) altitude acceptance for clean altitude starting point before landing
return _param_nav_fw_altl_rad.get();
}
}
return getDefaultAltAcceptanceRadiusMeter();
}

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@ -0,0 +1,157 @@
/***************************************************************************
*
* Copyright (c) 2013-2017 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
*/
#include <px4_platform_common/module_params.h>
#include <lib/mathlib/mathlib.h>
#include <uORB/topics/vehicle_local_position.h>
#include <uORB/topics/vehicle_status.h>
#include <uORB/topics/vehicle_global_position.h>
#include <uORB/topics/vehicle_land_detected.h>
#include <uORB/topics/home_position.h>
#include <uORB/topics/position_controller_status.h>
#include <uORB/topics/position_setpoint_triplet.h>
class NavigatorCore : public ModuleParams
{
public:
NavigatorCore();
~NavigatorCore();
typedef matrix::Vector3<float> Vector3f;
typedef matrix::Vector2<double> Vector2d;
bool getLanded() { return _landed_state.landed; }
bool getMaybeLanded() { return _landed_state.maybe_landed; }
float getLandDetectedAltMaxMeter() { return _landed_state.alt_max; }
double getLatRad() { return _global_pos.lat; }
double getLonRad() { return _global_pos.lon;}
float getAltitudeAMSLMeters() { return _global_pos.alt; }
float getTrueHeadingRad() { return _local_pos.heading; }
double getHomeLatRad() { return _home.lat; }
double getHomeLonRad() { return _home.lon; }
float getHomeAltAMSLMeter() { return _home.alt; }
float getHomeTrueHeadingRad() { return _home.yaw; }
home_position_s &getHomePosition() { return _home; }
bool isNotArmed() { return _status.arming_state != vehicle_status_s::ARMING_STATE_ARMED; }
uint8_t getArmingState() { return _status.arming_state; }
float getPosNorthMeter() { return _local_pos.x; }
float getPosEastMeter() { return _local_pos.y; }
float getPosDownMeter() { return _local_pos.z; }
float getVelNorthMPS() { return _local_pos.vx; }
float getVelEastMPS() { return _local_pos.vy; }
float getVelDownMPS() { return _local_pos.vz; }
float getLoiterRadiusMeter() { return _param_nav_loiter_rad.get(); }
bool getIsInTransitionMode() { return _status.in_transition_mode; }
position_setpoint_triplet_s getCurrentTriplet() { return _triplet; }
bool isHomeValid() { return (_home.timestamp > 0 && _home.valid_alt && _home.valid_hpos && _home.valid_lpos); }
bool isHomeAltValid() { return (_home.timestamp > 0 && _home.valid_alt); }
bool isRotaryWing() { return _status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING; }
bool isFixedWing() { return _status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_FIXED_WING; }
bool isRover() { return _status.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROVER; }
bool isVTOL() { return _status.is_vtol; }
uint8_t getVehicleType() { return _status.vehicle_type; }
float getDefaultAltAcceptanceRadiusMeter();
float getAltAcceptanceRadMeter();
float getFixedWingLandingAltAcceptanceRadius() { return _param_nav_fw_altl_rad.get(); }
float getDefaultHorAcceptanceRadiusMeter() { return _param_nav_acc_rad.get(); }
float getHorAcceptanceRadiusMeter();
float getMulticopterAltAcceptanceRadiusMeter() { return _param_nav_mc_alt_rad.get(); }
float getFixedWingAltAcceptanceRadiusMeter() { return _param_nav_fw_alt_rad.get(); }
float getAcceptanceRadiusMeter();
float getAltAcceptanceRadiusMeter();
float getRelativeTakeoffMinAltitudeMeter() { return _param_mis_takeoff_alt.get(); }
float getRelativeLoiterMinAltitudeMeter() { return _param_mis_ltrmin_alt.get(); }
bool isTakeoffRequired() { return _param_mis_takeoff_req.get(); }
float getWaypointHeadingTimeoutSeconds() { return _param_mis_yaw_tmt.get(); }
float getWaypointHeadingAcceptanceRad() { return _param_mis_yaw_err.get(); }
bool forceVTOL();
void updateLocalPosition(const vehicle_local_position_s &local_pos) { _local_pos = local_pos; };
void updateVehicleStatus(const vehicle_status_s &status) { _status = status; }
void updateGlobalPosition(const vehicle_global_position_s &global_pos) { _global_pos = global_pos; }
void updateLandedState(const vehicle_land_detected_s &landed_state) { _landed_state = landed_state; }
void updateHomePosition(const home_position_s &home) { _home = home; }
void updatePositionControllerStatus(const position_controller_status_s &pos_ctrl_status) { _pos_ctrl_status = pos_ctrl_status; }
private:
vehicle_local_position_s _local_pos{};
vehicle_status_s _status{};
vehicle_global_position_s _global_pos{};
vehicle_land_detected_s _landed_state{};
home_position_s _home{};
position_controller_status_s _pos_ctrl_status{};
position_setpoint_triplet_s _triplet{};
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
)
};

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@ -0,0 +1,121 @@
/****************************************************************************
*
* Copyright (C) 2021 PX4 Development Team. All rights reserved.
*
* Redistribution and use in source and binary forms, with or without
* modification, are permitted provided that the following conditions
* are met:
*
* 1. Redistributions of source code must retain the above copyright
* notice, this list of conditions and the following disclaimer.
* 2. Redistributions in binary form must reproduce the above copyright
* notice, this list of conditions and the following disclaimer in
* the documentation and/or other materials provided with the
* distribution.
* 3. Neither the name PX4 nor the names of its contributors may be
* used to endorse or promote products derived from this software
* without specific prior written permission.
*
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
#include <gtest/gtest.h>
#include "FakeNavigator.h"
#include "takeoff.h"
#include <dataman/dataman_mocks.hpp>
TEST(NavigatorModeTakeoffTest, TestTakeoff)
{
FakeNavigator fake_navigator;
NavigatorCore &navigator_core = fake_navigator.getCore();
Takeoff takeoff(&fake_navigator, navigator_core);
fake_navigator.params_update();
vehicle_status_s status = {};
status.timestamp = 1e6;
status.is_vtol = true;
status.arming_state = vehicle_status_s::ARMING_STATE_ARMED;
status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
vehicle_global_position_s global_pos = {};
global_pos.timestamp = 1e6;
global_pos.lat = 40;
global_pos.lon = 3;
global_pos.alt = 300;
vehicle_land_detected_s landed = {};
landed.landed = true;
landed.timestamp = 1e6;
home_position_s home = {};
home.timestamp = 1e6;
home.lat = global_pos.lat;
home.lon = global_pos.lon;
home.alt = global_pos.alt;
home.valid_alt = true;
home.valid_hpos = true;
home.valid_lpos = true;
vehicle_local_position_s local_pos = {};
local_pos.timestamp = 1e6;
local_pos.x = -0.2f;
local_pos.y = 0.1f;
local_pos.z = 0.1f;
local_pos.vx = local_pos.vy = local_pos.vz = 0;
local_pos.heading = -0.54f;
navigator_core.updateGlobalPosition(global_pos);
navigator_core.updateHomePosition(home);
navigator_core.updateLandedState(landed);
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);
}

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@ -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{};

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@ -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;

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@ -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;

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@ -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;

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@ -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;

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@ -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;

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@ -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 {

View File

@ -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;

View File

@ -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);

View File

@ -46,7 +46,7 @@
class Land : public MissionBlock
{
public:
Land(Navigator *navigator);
Land(Navigator *navigator, NavigatorCore &navigator_core);
~Land() = default;
void on_activation() override;

View File

@ -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;

View File

@ -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;

View File

@ -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) {

View File

@ -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;

View File

@ -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;

View File

@ -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)};
};

View File

@ -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) {

View File

@ -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

View File

@ -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[])
{

View File

@ -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;

View File

@ -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;

View File

@ -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

View File

@ -72,7 +72,7 @@ public:
RTL_DESTINATION_SAFE_POINT,
};
RTL(Navigator *navigator);
RTL(Navigator *navigator, NavigatorCore &navigator_core);
~RTL() = default;

View File

@ -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");
}

View File

@ -46,7 +46,7 @@
class Takeoff : public MissionBlock
{
public:
Takeoff(Navigator *navigator);
Takeoff(Navigator *navigator, NavigatorCore &navigator_core);
~Takeoff() = default;
void on_activation() override;