10#include <px4_msgs/msg/fixed_wing_lateral_setpoint.hpp>
11#include <px4_msgs/msg/fixed_wing_longitudinal_setpoint.hpp>
12#include <px4_msgs/msg/lateral_control_configuration.hpp>
13#include <px4_msgs/msg/longitudinal_control_configuration.hpp>
14#include <px4_ros2/common/exception.hpp>
15#include <px4_ros2/common/setpoint_base.hpp>
22struct FwLateralLongitudinalSetpoint;
23struct FwControlConfiguration;
88 std::optional<float> equivalent_airspeed_sp = {},
89 std::optional<float> lateral_acceleration_sp = {});
100 std::optional<float> equivalent_airspeed_sp = {},
101 std::optional<float> lateral_acceleration_sp = {});
103 float desiredUpdateRateHz()
override {
return 30.f; }
107 bool _local_position_is_optional;
108 rclcpp::Publisher<px4_msgs::msg::FixedWingLateralSetpoint>::SharedPtr _fw_lateral_sp_pub;
109 rclcpp::Publisher<px4_msgs::msg::FixedWingLongitudinalSetpoint>::SharedPtr
110 _fw_longitudinal_sp_pub;
112 rclcpp::Publisher<px4_msgs::msg::LateralControlConfiguration>::SharedPtr
113 _lateral_control_configuration_pub;
114 rclcpp::Publisher<px4_msgs::msg::LongitudinalControlConfiguration>::SharedPtr
115 _longitudinal_control_configuration_pub;
119 std::optional<float> course;
120 std::optional<float> airspeed_direction;
121 std::optional<float> lateral_acceleration;
122 std::optional<float> altitude_msl;
123 std::optional<float> height_rate;
124 std::optional<float> equivalent_airspeed;
125 std::optional<float> throttle_direct;
135 airspeed_direction = airspeed_direction_sp;
141 lateral_acceleration = lateral_acceleration_sp;
147 altitude_msl = altitude_sp;
153 height_rate = height_rate_sp;
159 equivalent_airspeed = equivalent_airspeed_sp;
165 throttle_direct = throttle_direct_sp;
171 std::optional<float> min_pitch;
172 std::optional<float> max_pitch;
173 std::optional<float> min_throttle;
174 std::optional<float> max_throttle;
175 std::optional<float> max_lateral_acceleration;
176 std::optional<float> target_climb_rate;
177 std::optional<float> target_sink_rate;
178 std::optional<float> speed_weight;
182 min_pitch = min_pitch_sp;
183 max_pitch = max_pitch_sp;
190 min_throttle = min_throttle_sp;
191 max_throttle = max_throttle_sp;
198 max_lateral_acceleration = max_lateral_acceleration_sp;
204 target_sink_rate = target_sink_rate_sp;
210 target_climb_rate = target_climb_rate_sp;
224 if (speed_weight_sp < 0.0 || speed_weight_sp > 2.0) {
225 throw Exception(
"Speed weight must be between 0 and 2.");
227 speed_weight = speed_weight_sp;
Definition context.hpp:18
Definition exception.hpp:14
Setpoint type for fixedwing control.
Definition lateral_longitudinal.hpp:28
FwLateralLongitudinalSetpointType(Context &context, bool is_position_optional=false)
void updateWithAltitude(float altitude_amsl_sp, float course_sp, std::optional< float > equivalent_airspeed_sp={}, std::optional< float > lateral_acceleration_sp={})
Update the setpoint with simplest set of inputs: Altitude and Course. Lateral acceleration setpoints ...
void update(const FwLateralLongitudinalSetpoint &setpoint)
Update the setpoint with full flexibility by passing a FwLateralLongitudinalSetpoint.
void update(const FwLateralLongitudinalSetpoint &setpoint, const FwControlConfiguration &config)
Update the setpoint with full flexibility by passing a FwLateralLongitudinalSetpoint and FwControlCon...
void updateWithHeightRate(float height_rate_sp, float course_sp, std::optional< float > equivalent_airspeed_sp={}, std::optional< float > lateral_acceleration_sp={})
Update the setpoint with simplest set of inputs: Height rate and Course. Lateral acceleration setpoin...
Definition setpoint_base.hpp:19
Definition lateral_longitudinal.hpp:170
FwControlConfiguration & withSpeedWeight(float speed_weight_sp)
Configure the speed weight for TECS (Total Energy Control System). For more information on TECS,...
Definition lateral_longitudinal.hpp:222
Definition lateral_longitudinal.hpp:118
Definition setpoint_base.hpp:23