/**************************************************************************** * * Copyright (c) 2013-2019 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 #include "ecl_pitch_controller.h" #include "ecl_roll_controller.h" #include "ecl_wheel_controller.h" #include "ecl_yaw_controller.h" #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include #include using matrix::Eulerf; using matrix::Quatf; using uORB::SubscriptionData; using namespace time_literals; class FixedwingAttitudeControl final : public ModuleBase, public ModuleParams, public px4::WorkItem { public: FixedwingAttitudeControl(bool vtol = false); ~FixedwingAttitudeControl() override; /** @see ModuleBase */ static int task_spawn(int argc, char *argv[]); /** @see ModuleBase */ static int custom_command(int argc, char *argv[]); /** @see ModuleBase */ static int print_usage(const char *reason = nullptr); bool init(); private: void Run() override; uORB::SubscriptionCallbackWorkItem _att_sub{this, ORB_ID(vehicle_attitude)}; /**< vehicle attitude */ uORB::SubscriptionInterval _parameter_update_sub{ORB_ID(parameter_update), 1_s}; uORB::Subscription _att_sp_sub{ORB_ID(vehicle_attitude_setpoint)}; /**< vehicle attitude setpoint */ uORB::Subscription _battery_status_sub{ORB_ID(battery_status)}; /**< battery status subscription */ uORB::Subscription _local_pos_sub{ORB_ID(vehicle_local_position)}; /**< local position subscription */ uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)}; /**< notification of manual control updates */ uORB::Subscription _rates_sp_sub{ORB_ID(vehicle_rates_setpoint)}; /**< vehicle rates setpoint */ uORB::Subscription _vcontrol_mode_sub{ORB_ID(vehicle_control_mode)}; /**< vehicle status subscription */ uORB::Subscription _vehicle_land_detected_sub{ORB_ID(vehicle_land_detected)}; /**< vehicle land detected subscription */ uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)}; /**< vehicle status subscription */ uORB::Subscription _vehicle_rates_sub{ORB_ID(vehicle_angular_velocity)}; uORB::SubscriptionData _airspeed_validated_sub{ORB_ID(airspeed_validated)}; uORB::Publication _actuators_0_pub; uORB::Publication _attitude_sp_pub; uORB::Publication _rate_sp_pub{ORB_ID(vehicle_rates_setpoint)}; uORB::PublicationMulti _rate_ctrl_status_pub{ORB_ID(rate_ctrl_status)}; actuator_controls_s _actuators {}; /**< actuator control inputs */ manual_control_setpoint_s _manual_control_setpoint {}; /**< r/c channel data */ vehicle_attitude_setpoint_s _att_sp {}; /**< vehicle attitude setpoint */ vehicle_control_mode_s _vcontrol_mode {}; /**< vehicle control mode */ vehicle_local_position_s _local_pos {}; /**< local position */ vehicle_rates_setpoint_s _rates_sp {}; /* attitude rates setpoint */ vehicle_status_s _vehicle_status {}; /**< vehicle status */ perf_counter_t _loop_perf; /**< loop performance counter */ hrt_abstime _last_run{0}; float _flaps_applied{0.0f}; float _flaperons_applied{0.0f}; float _airspeed_scaling{1.0f}; bool _landed{true}; float _battery_scale{1.0f}; bool _flag_control_attitude_enabled_last{false}; bool _is_tailsitter{false}; DEFINE_PARAMETERS( (ParamFloat) _param_fw_acro_x_max, (ParamFloat) _param_fw_acro_y_max, (ParamFloat) _param_fw_acro_z_max, (ParamFloat) _param_fw_airspd_max, (ParamFloat) _param_fw_airspd_min, (ParamFloat) _param_fw_airspd_trim, (ParamInt) _param_fw_arsp_mode, (ParamInt) _param_fw_arsp_scale_en, (ParamBool) _param_fw_bat_scale_en, (ParamFloat) _param_fw_dtrim_p_flps, (ParamFloat) _param_fw_dtrim_p_vmax, (ParamFloat) _param_fw_dtrim_p_vmin, (ParamFloat) _param_fw_dtrim_r_flps, (ParamFloat) _param_fw_dtrim_r_vmax, (ParamFloat) _param_fw_dtrim_r_vmin, (ParamFloat) _param_fw_dtrim_y_vmax, (ParamFloat) _param_fw_dtrim_y_vmin, (ParamFloat) _param_fw_flaperon_scl, (ParamFloat) _param_fw_flaps_lnd_scl, (ParamFloat) _param_fw_flaps_scl, (ParamFloat) _param_fw_flaps_to_scl, (ParamFloat) _param_fw_man_p_max, (ParamFloat) _param_fw_man_p_sc, (ParamFloat) _param_fw_man_r_max, (ParamFloat) _param_fw_man_r_sc, (ParamFloat) _param_fw_man_y_sc, (ParamFloat) _param_fw_p_rmax_neg, (ParamFloat) _param_fw_p_rmax_pos, (ParamFloat) _param_fw_p_tc, (ParamFloat) _param_fw_pr_ff, (ParamFloat) _param_fw_pr_i, (ParamFloat) _param_fw_pr_imax, (ParamFloat) _param_fw_pr_p, (ParamFloat) _param_fw_psp_off, (ParamFloat) _param_fw_r_rmax, (ParamFloat) _param_fw_r_tc, (ParamFloat) _param_fw_rll_to_yaw_ff, (ParamFloat) _param_fw_rr_ff, (ParamFloat) _param_fw_rr_i, (ParamFloat) _param_fw_rr_imax, (ParamFloat) _param_fw_rr_p, (ParamBool) _param_fw_w_en, (ParamFloat) _param_fw_w_rmax, (ParamFloat) _param_fw_wr_ff, (ParamFloat) _param_fw_wr_i, (ParamFloat) _param_fw_wr_imax, (ParamFloat) _param_fw_wr_p, (ParamFloat) _param_fw_y_rmax, (ParamFloat) _param_fw_yr_ff, (ParamFloat) _param_fw_yr_i, (ParamFloat) _param_fw_yr_imax, (ParamFloat) _param_fw_yr_p, (ParamFloat) _param_trim_pitch, (ParamFloat) _param_trim_roll, (ParamFloat) _param_trim_yaw ) ECL_RollController _roll_ctrl; ECL_PitchController _pitch_ctrl; ECL_YawController _yaw_ctrl; ECL_WheelController _wheel_ctrl; void control_flaps(const float dt); /** * Update our local parameter cache. */ int parameters_update(); void vehicle_control_mode_poll(); void vehicle_manual_poll(); void vehicle_attitude_setpoint_poll(); void vehicle_rates_setpoint_poll(); void vehicle_land_detected_poll(); float get_airspeed_and_update_scaling(); };