/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /* Lead developers: Matthew Ridley and Andrew Tridgell Please contribute your ideas! See http://dev.ardupilot.org for details This program is free software: you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation, either version 3 of the License, or (at your option) any later version. This program is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. You should have received a copy of the GNU General Public License along with this program. If not, see . */ #pragma once //////////////////////////////////////////////////////////////////////////////// // Header includes //////////////////////////////////////////////////////////////////////////////// #include #include #include #include #include #include #include #include // ArduPilot GPS library #include // ArduPilot barometer library #include // ArduPilot Mega Magnetometer Library #include // ArduPilot Mega Vector/Matrix math Library #include // ArduPilot Mega Analog to Digital Converter Library #include // Inertial Sensor Library #include // interface and maths for accelerometer calibration #include // ArduPilot Mega DCM Library #include // Filter library #include // APM FIFO Buffer #include // Serial manager library #include // ArduPilot Mega Declination Helper Library #include #include #include // main loop scheduler #include #include #include #include #include #include #include // Notify library #include // Battery monitor library #include #include #include #include #include // Configuration #include "config.h" #include "defines.h" #include "Parameters.h" #include "GCS_Mavlink.h" #if CONFIG_HAL_BOARD == HAL_BOARD_SITL #include #endif class Tracker : public AP_HAL::HAL::Callbacks { public: friend class GCS_MAVLINK_Tracker; friend class Parameters; Tracker(void); // HAL::Callbacks implementation. void setup() override; void loop() override; private: Parameters g; // main loop scheduler AP_Scheduler scheduler; // notification object for LEDs, buzzers etc AP_Notify notify; uint32_t start_time_ms = 0; bool usb_connected = false; // has a log download started? bool in_log_download = false; bool logging_started = false; DataFlash_Class DataFlash; AP_GPS gps; AP_Baro barometer; Compass compass; AP_InertialSensor ins; RangeFinder rng {serial_manager}; // Inertial Navigation EKF #if AP_AHRS_NAVEKF_AVAILABLE NavEKF EKF{&ahrs, barometer, rng}; NavEKF2 EKF2{&ahrs, barometer, rng}; AP_AHRS_NavEKF ahrs{ins, barometer, gps, rng, EKF, EKF2}; #else AP_AHRS_DCM ahrs{ins, barometer, gps}; #endif #if CONFIG_HAL_BOARD == HAL_BOARD_SITL SITL::SITL sitl; #endif /** antenna control channels */ RC_Channel channel_yaw{CH_YAW}; RC_Channel channel_pitch{CH_PITCH}; AP_SerialManager serial_manager; const uint8_t num_gcs = MAVLINK_COMM_NUM_BUFFERS; GCS_MAVLINK_Tracker gcs[MAVLINK_COMM_NUM_BUFFERS]; AP_BoardConfig BoardConfig; struct Location current_loc; enum ControlMode control_mode = INITIALISING; // Vehicle state struct { bool location_valid; // true if we have a valid location for the vehicle Location location; // lat, long in degrees * 10^7; alt in meters * 100 Location location_estimate; // lat, long in degrees * 10^7; alt in meters * 100 uint32_t last_update_us; // last position update in microseconds uint32_t last_update_ms; // last position update in milliseconds Vector3f vel; // the vehicle's velocity in m/s int32_t relative_alt; // the vehicle's relative altitude in meters * 100 } vehicle; // Navigation controller state struct { float bearing; // bearing to vehicle in centi-degrees float distance; // distance to vehicle in meters float pitch; // pitch to vehicle in degrees (positive means vehicle is above tracker, negative means below) float alt_difference_baro; // altitude difference between tracker and vehicle in meters according to the barometer. positive value means vehicle is above tracker float alt_difference_gps; // altitude difference between tracker and vehicle in meters according to the gps. positive value means vehicle is above tracker float altitude_offset; // offset in meters which is added to tracker altitude to align altitude measurements with vehicle's barometer bool manual_control_yaw : 1;// true if tracker yaw is under manual control bool manual_control_pitch : 1;// true if tracker pitch is manually controlled bool need_altitude_calibration : 1;// true if tracker altitude has not been determined (true after startup) bool scan_reverse_pitch : 1;// controls direction of pitch movement in SCAN mode bool scan_reverse_yaw : 1;// controls direction of yaw movement in SCAN mode } nav_status = {0.0f, 0.0f, 0.0f, 0.0f, 0.0f, 0.0f, false, false, true, false, false}; // setup the var_info table AP_Param param_loader{var_info}; uint8_t one_second_counter = 0; bool target_set = false; int8_t slew_dir = 0; uint32_t slew_start_ms = 0; // use this to prevent recursion during sensor init bool in_mavlink_delay = false; static const AP_Scheduler::Task scheduler_tasks[]; static const AP_Param::Info var_info[]; static const struct LogStructure log_structure[]; void dataflash_periodic(void); void one_second_loop(); void ten_hz_logging_loop(); void send_heartbeat(mavlink_channel_t chan); void send_attitude(mavlink_channel_t chan); void send_location(mavlink_channel_t chan); void send_radio_out(mavlink_channel_t chan); void send_hwstatus(mavlink_channel_t chan); void send_waypoint_request(mavlink_channel_t chan); void send_nav_controller_output(mavlink_channel_t chan); void send_simstate(mavlink_channel_t chan); void mavlink_check_target(const mavlink_message_t* msg); void gcs_send_message(enum ap_message id); void gcs_data_stream_send(void); void gcs_update(void); void gcs_send_text(MAV_SEVERITY severity, const char *str); void gcs_retry_deferred(void); void load_parameters(void); void update_auto(void); void update_manual(void); void update_scan(void); bool servo_test_set_servo(uint8_t servo_num, uint16_t pwm); void read_radio(); void init_barometer(bool full_calibration); void update_barometer(void); void update_ahrs(); void update_compass(void); void compass_accumulate(void); void accel_cal_update(void); void barometer_accumulate(void); void update_GPS(void); void init_servos(); void update_pitch_servo(float pitch); void update_pitch_position_servo(float pitch); void update_pitch_cr_servo(float pitch); void update_pitch_onoff_servo(float pitch); void update_yaw_servo(float yaw); void update_yaw_position_servo(float yaw); void update_yaw_cr_servo(float yaw); void update_yaw_onoff_servo(float yaw); void init_tracker(); void update_notify(); bool get_home_eeprom(struct Location &loc); void set_home_eeprom(struct Location temp); void set_home(struct Location temp); void arm_servos(); void disarm_servos(); void prepare_servos(); void set_mode(enum ControlMode mode); bool mavlink_set_mode(uint8_t mode); void check_usb_mux(void); void update_vehicle_pos_estimate(); void update_tracker_position(); void update_bearing_and_distance(); void update_tracking(void); void tracking_update_position(const mavlink_global_position_int_t &msg); void tracking_update_pressure(const mavlink_scaled_pressure_t &msg); void tracking_manual_control(const mavlink_manual_control_t &msg); void update_armed_disarmed(); void gcs_send_text_fmt(MAV_SEVERITY severity, const char *fmt, ...); void init_capabilities(void); void compass_cal_update(); void Log_Write_Attitude(); void Log_Write_Baro(void); void Log_Write_Vehicle_Pos(int32_t lat,int32_t lng,int32_t alt, const Vector3f& vel); void Log_Write_Vehicle_Baro(float pressure, float altitude); void Log_Write_Vehicle_Startup_Messages(); void start_logging(); void log_init(void); bool should_log(uint32_t mask); public: void mavlink_snoop(const mavlink_message_t* msg); void mavlink_delay_cb(); }; #define MENU_FUNC(func) FUNCTOR_BIND(&tracker, &Tracker::func, int8_t, uint8_t, const Menu::arg *) extern const AP_HAL::HAL& hal; extern Tracker tracker;