/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #define THISFIRMWARE "AntennaTracker V0.5" /* Lead developers: Matthew Ridley and Andrew Tridgell Please contribute your ideas! See http://dev.ardupilot.com 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 . */ //////////////////////////////////////////////////////////////////////////////// // Header includes //////////////////////////////////////////////////////////////////////////////// #include #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 #include // Inertial Sensor Library #include // ArduPilot Mega DCM Library #include // Filter library #include // APM FIFO Buffer #include #include // MAVLink GCS definitions #include // Serial manager library #include // ArduPilot Mega Declination Helper Library #include #include #include #include // main loop scheduler #include #include #include #include #include #include // Notify library #include // Battery monitor library #include #include #include #include #include // Configuration #include "config.h" // Local modules #include "defines.h" #include "Parameters.h" #include "GCS.h" #include #include #include #include #include #include AP_HAL::BetterStream* cliSerial; const AP_HAL::HAL& hal = AP_HAL_BOARD_DRIVER; //////////////////////////////////////////////////////////////////////////////// // the rate we run the main loop at //////////////////////////////////////////////////////////////////////////////// static const AP_InertialSensor::Sample_rate ins_sample_rate = AP_InertialSensor::RATE_50HZ; //////////////////////////////////////////////////////////////////////////////// // Parameters //////////////////////////////////////////////////////////////////////////////// // // Global parameters are all contained within the 'g' class. // static Parameters g; // main loop scheduler static AP_Scheduler scheduler; // notification object for LEDs, buzzers etc static AP_Notify notify; static uint32_t start_time_ms; static bool usb_connected; //////////////////////////////////////////////////////////////////////////////// // prototypes void gcs_send_text_fmt(const prog_char_t *fmt, ...); //////////////////////////////////////////////////////////////////////////////// // Sensors //////////////////////////////////////////////////////////////////////////////// static AP_GPS gps; static AP_Baro barometer; static Compass compass; #if CONFIG_HAL_BOARD == HAL_BOARD_APM1 AP_ADC_ADS7844 apm1_adc; #endif AP_InertialSensor ins; static RangeFinder rng; // Inertial Navigation EKF #if AP_AHRS_NAVEKF_AVAILABLE AP_AHRS_NavEKF ahrs(ins, barometer, gps, rng); #else AP_AHRS_DCM ahrs(ins, barometer, gps); #endif #if CONFIG_HAL_BOARD == HAL_BOARD_SITL SITL sitl; #endif /** antenna control channels */ static RC_Channel channel_yaw(CH_YAW); static RC_Channel channel_pitch(CH_PITCH); //////////////////////////////////////////////////////////////////////////////// // GCS selection //////////////////////////////////////////////////////////////////////////////// static AP_SerialManager serial_manager; static const uint8_t num_gcs = MAVLINK_COMM_NUM_BUFFERS; static GCS_MAVLINK gcs[MAVLINK_COMM_NUM_BUFFERS]; // board specific config static AP_BoardConfig BoardConfig; //////////////////////////////////////////////////////////////////////////////// // 3D Location vectors // Location structure defined in AP_Common //////////////////////////////////////////////////////////////////////////////// static struct Location current_loc; // This is the state of the antenna control system // There are multiple states defined such as MANUAL, FBW-A, AUTO static enum ControlMode control_mode = INITIALISING; //////////////////////////////////////////////////////////////////////////////// // Vehicle state //////////////////////////////////////////////////////////////////////////////// static 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 micxroseconds uint32_t last_update_ms; // last position update in milliseconds float heading; // last known direction vehicle is moving float ground_speed; // vehicle's last known ground speed in m/s } vehicle; //////////////////////////////////////////////////////////////////////////////// // Navigation controller state //////////////////////////////////////////////////////////////////////////////// static 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 altitude_difference; // altitude difference between tracker and vehicle in meters. 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; //////////////////////////////////////////////////////////////////////////////// // Servo state //////////////////////////////////////////////////////////////////////////////// static struct { bool yaw_lower : 1; // true if yaw servo has been limited from moving to a lower position (i.e. position or rate limited) bool yaw_upper : 1; // true if yaw servo has been limited from moving to a higher position (i.e. position or rate limited) bool pitch_lower : 1; // true if pitch servo has been limited from moving to a lower position (i.e. position or rate limited) bool pitch_upper : 1; // true if pitch servo has been limited from moving to a higher position (i.e. position or rate limited) } servo_limit; /* scheduler table - all regular tasks apart from the fast_loop() should be listed here, along with how often they should be called (in 20ms units) and the maximum time they are expected to take (in microseconds) */ static const AP_Scheduler::Task scheduler_tasks[] PROGMEM = { { update_ahrs, 1, 1000 }, { read_radio, 1, 200 }, { update_tracking, 1, 1000 }, { update_GPS, 5, 4000 }, { update_compass, 5, 1500 }, { update_barometer, 5, 1500 }, { gcs_update, 1, 1700 }, { gcs_data_stream_send, 1, 3000 }, { compass_accumulate, 1, 1500 }, { barometer_accumulate, 1, 900 }, { update_notify, 1, 100 }, { check_usb_mux, 5, 300 }, { gcs_retry_deferred, 1, 1000 }, { one_second_loop, 50, 3900 } }; // setup the var_info table AP_Param param_loader(var_info); /** setup the sketch - called once on startup */ void setup() { cliSerial = hal.console; // load the default values of variables listed in var_info[] AP_Param::setup_sketch_defaults(); // initialise notify notify.init(false); // antenna tracker does not use pre-arm checks or battery failsafe AP_Notify::flags.pre_arm_check = true; AP_Notify::flags.pre_arm_gps_check = true; AP_Notify::flags.failsafe_battery = false; init_tracker(); // initialise the main loop scheduler scheduler.init(&scheduler_tasks[0], sizeof(scheduler_tasks)/sizeof(scheduler_tasks[0])); } /** loop() is called continuously */ void loop() { // wait for an INS sample ins.wait_for_sample(); // tell the scheduler one tick has passed scheduler.tick(); scheduler.run(19900UL); } static void one_second_loop() { // send a heartbeat gcs_send_message(MSG_HEARTBEAT); // make it possible to change orientation at runtime ahrs.set_orientation(); // sync MAVLink system ID mavlink_system.sysid = g.sysid_this_mav; // updated armed/disarmed status LEDs update_armed_disarmed(); static uint8_t counter; counter++; if (counter >= 60) { if(g.compass_enabled) { compass.save_offsets(); } counter = 0; } } AP_HAL_MAIN();