/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /* ArduCopter Version 2.0 Beta Authors: Jason Short Based on code and ideas from the Arducopter team: Jose Julio, Randy Mackay, Jani Hirvinen Thanks to: Chris Anderson, Mike Smith, Jordi Munoz, Doug Weibel, James Goppert, Benjamin Pelletier This firmware is free software; you can redistribute it and/or modify it under the terms of the GNU Lesser General Public License as published by the Free Software Foundation; either version 2.1 of the License, or (at your option) any later version. */ //////////////////////////////////////////////////////////////////////////////// // Header includes //////////////////////////////////////////////////////////////////////////////// // AVR runtime #include #include #include #include // Libraries #include #include #include // ArduPilot Mega RC Library #include // ArduPilot GPS library #include // Arduino I2C lib #include #include // ArduPilot Mega Flash Memory Library #include // ArduPilot Mega Analog to Digital Converter Library #include // ArduPilot Mega BMP085 Library #include // ArduPilot Mega Magnetometer Library #include // ArduPilot Mega Vector/Matrix math Library #include // ArduPilot Mega IMU Library #include // ArduPilot Mega DCM Library #include // PID library #include // RC Channel Library #include // Range finder library #define MAVLINK_COMM_NUM_BUFFERS 2 #include // MAVLink GCS definitions // Configuration #include "config.h" // Local modules #include "defines.h" #include "Parameters.h" #include "GCS.h" #include "HIL.h" //////////////////////////////////////////////////////////////////////////////// // Serial ports //////////////////////////////////////////////////////////////////////////////// // // Note that FastSerial port buffers are allocated at ::begin time, // so there is not much of a penalty to defining ports that we don't // use. // FastSerialPort0(Serial); // FTDI/console FastSerialPort1(Serial1); // GPS port FastSerialPort3(Serial3); // Telemetry port //////////////////////////////////////////////////////////////////////////////// // Parameters //////////////////////////////////////////////////////////////////////////////// // // Global parameters are all contained within the 'g' class. // Parameters g; //////////////////////////////////////////////////////////////////////////////// // prototypes void update_events(void); //////////////////////////////////////////////////////////////////////////////// // Sensors //////////////////////////////////////////////////////////////////////////////// // // There are three basic options related to flight sensor selection. // // - Normal flight mode. Real sensors are used. // - HIL Attitude mode. Most sensors are disabled, as the HIL // protocol supplies attitude information directly. // - HIL Sensors mode. Synthetic sensors are configured that // supply data from the simulation. // // All GPS access should be through this pointer. GPS *g_gps; #if HIL_MODE == HIL_MODE_DISABLED // real sensors AP_ADC_ADS7844 adc; APM_BMP085_Class barometer; // MAG PROTOCOL #if MAG_PROTOCOL == MAG_PROTOCOL_5843 AP_Compass_HMC5843 compass(Parameters::k_param_compass); #elif MAG_PROTOCOL == MAG_PROTOCOL_5883L AP_Compass_HMC5883L compass(Parameters::k_param_compass); #else #error Unrecognised MAG_PROTOCOL setting. #endif // real GPS selection #if GPS_PROTOCOL == GPS_PROTOCOL_AUTO AP_GPS_Auto g_gps_driver(&Serial1, &g_gps); #elif GPS_PROTOCOL == GPS_PROTOCOL_NMEA AP_GPS_NMEA g_gps_driver(&Serial1); #elif GPS_PROTOCOL == GPS_PROTOCOL_SIRF AP_GPS_SIRF g_gps_driver(&Serial1); #elif GPS_PROTOCOL == GPS_PROTOCOL_UBLOX AP_GPS_UBLOX g_gps_driver(&Serial1); #elif GPS_PROTOCOL == GPS_PROTOCOL_MTK AP_GPS_MTK g_gps_driver(&Serial1); #elif GPS_PROTOCOL == GPS_PROTOCOL_MTK16 AP_GPS_MTK16 g_gps_driver(&Serial1); #elif GPS_PROTOCOL == GPS_PROTOCOL_NONE AP_GPS_None g_gps_driver(NULL); #else #error Unrecognised GPS_PROTOCOL setting. #endif // GPS PROTOCOL #elif HIL_MODE == HIL_MODE_SENSORS // sensor emulators AP_ADC_HIL adc; APM_BMP085_HIL_Class barometer; AP_Compass_HIL compass; AP_GPS_HIL g_gps_driver(NULL); #elif HIL_MODE == HIL_MODE_ATTITUDE AP_DCM_HIL dcm; AP_GPS_HIL g_gps_driver(NULL); AP_Compass_HIL compass; // never used AP_IMU_Shim imu; // never used #else #error Unrecognised HIL_MODE setting. #endif // HIL MODE #if HIL_MODE != HIL_MODE_DISABLED #if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK GCS_MAVLINK hil(Parameters::k_param_streamrates_port0); #elif HIL_PROTOCOL == HIL_PROTOCOL_XPLANE HIL_XPLANE hil; #endif // HIL PROTOCOL #endif // HIL_MODE // We may have a hil object instantiated just for mission planning #if HIL_MODE == HIL_MODE_DISABLED && HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && HIL_PORT == 0 GCS_MAVLINK hil(Parameters::k_param_streamrates_port0); #endif #if HIL_MODE != HIL_MODE_ATTITUDE #if HIL_MODE != HIL_MODE_SENSORS // Normal AP_IMU_Oilpan imu(&adc, Parameters::k_param_IMU_calibration); #else // hil imu AP_IMU_Shim imu; #endif // normal dcm AP_DCM dcm(&imu, g_gps); #endif //////////////////////////////////////////////////////////////////////////////// // GCS selection //////////////////////////////////////////////////////////////////////////////// // #if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK GCS_MAVLINK gcs(Parameters::k_param_streamrates_port3); #else // If we are not using a GCS, we need a stub that does nothing. GCS_Class gcs; #endif //#include //GCS_SIMPLE gcs_simple(&Serial); //////////////////////////////////////////////////////////////////////////////// // SONAR selection //////////////////////////////////////////////////////////////////////////////// // #if SONAR_TYPE == MAX_SONAR_XL AP_RangeFinder_MaxsonarXL sonar;//(SONAR_PORT, &adc); #elif SONAR_TYPE == MAX_SONAR_LV AP_RangeFinder_MaxsonarLV sonar;//(SONAR_PORT, &adc); #endif //////////////////////////////////////////////////////////////////////////////// // Global variables //////////////////////////////////////////////////////////////////////////////// byte control_mode = STABILIZE; byte oldSwitchPosition; // for remembering the control mode switch const char *comma = ","; const char* flight_mode_strings[] = { "STABILIZE", "ACRO", "ALT_HOLD", "SIMPLE", "AUTO", "GCS_AUTO", "LOITER", "RTL"}; /* Radio values Channel assignments 1 Ailerons (rudder if no ailerons) 2 Elevator 3 Throttle 4 Rudder (if we have ailerons) 5 Mode - 3 position switch 6 User assignable 7 trainer switch - sets throttle nominal (toggle switch), sets accels to Level (hold > 1 second) 8 TBD */ // Radio // ----- int motor_out[8]; Vector3f omega; // Heli // ---- float heli_rollFactor[3], heli_pitchFactor[3]; // only required for 3 swashplate servos int heli_servo_min[3], heli_servo_max[3]; // same here. for yaw servo we use heli_servo4_min/max parameter directly int heli_servo_out[4]; // Failsafe // -------- boolean failsafe; // did our throttle dip below the failsafe value? boolean ch3_failsafe; boolean motor_armed; boolean motor_auto_armed; // if true, // PIDs // ---- //int max_stabilize_dampener; // //int max_yaw_dampener; // boolean rate_yaw_flag; // used to transition yaw control from Rate control to Yaw hold byte yaw_debug; bool did_clear_yaw_control; // LED output // ---------- boolean motor_light; // status of the Motor safety boolean GPS_light; // status of the GPS light boolean timer_light; // status of the Motor safety byte led_mode = NORMAL_LEDS; // GPS variables // ------------- const float t7 = 10000000.0; // used to scale GPS values for EEPROM storage float scaleLongUp = 1; // used to reverse longtitude scaling float scaleLongDown = 1; // used to reverse longtitude scaling byte ground_start_count = 10; // have we achieved first lock and set Home? // Location & Navigation // --------------------- const float radius_of_earth = 6378100; // meters const float gravity = 9.81; // meters/ sec^2 long nav_bearing; // deg * 100 : 0 to 360 current desired bearing to navigate long target_bearing; // deg * 100 : 0 to 360 location of the plane to the target long crosstrack_bearing; // deg * 100 : 0 to 360 desired angle of plane to target int climb_rate; // m/s * 100 - For future implementation of controlled ascent/descent by rate float nav_gain_scaler = 1; // Gain scaling for headwind/tailwind TODO: why does this variable need to be initialized to 1? int last_ground_speed; // used to dampen navigation byte wp_control; // used to control - navgation or loiter byte command_must_index; // current command memory location byte command_may_index; // current command memory location byte command_must_ID; // current command ID byte command_may_ID; // current command ID byte wp_verify_byte; // used for tracking state of navigating waypoints float cos_roll_x = 1; float cos_pitch_x = 1; float cos_yaw_x = 1; float sin_pitch_y, sin_yaw_y, sin_roll_y; float sin_nav_y, cos_nav_x; // used in calc_nav_output XXX move to local funciton bool simple_bearing_is_set = false; long initial_simple_bearing; // used for Simple mode float Y6_scaling = Y6_MOTOR_SCALER; // Airspeed // -------- int airspeed; // m/s * 100 // Location Errors // --------------- long bearing_error; // deg * 100 : 0 to 36000 long altitude_error; // meters * 100 we are off in altitude float crosstrack_error; // meters we are off trackline long distance_error; // distance to the WP long yaw_error; // how off are we pointed long long_error, lat_error; // temp for debugging // Battery Sensors // --------------- float battery_voltage = LOW_VOLTAGE * 1.05; // Battery Voltage of total battery, initialized above threshold for filter float battery_voltage1 = LOW_VOLTAGE * 1.05; // Battery Voltage of cell 1, initialized above threshold for filter float battery_voltage2 = LOW_VOLTAGE * 1.05; // Battery Voltage of cells 1 + 2, initialized above threshold for filter float battery_voltage3 = LOW_VOLTAGE * 1.05; // Battery Voltage of cells 1 + 2+3, initialized above threshold for filter float battery_voltage4 = LOW_VOLTAGE * 1.05; // Battery Voltage of cells 1 + 2+3 + 4, initialized above threshold for filter float current_amps; float current_total; // Airspeed Sensors // ---------------- // Barometer Sensor variables // -------------------------- long abs_pressure; long ground_pressure; int ground_temperature; int32_t baro_filter[BARO_FILTER_SIZE]; byte baro_filter_index; // Altitude Sensor variables // ---------------------- int sonar_alt; int baro_alt; int baro_alt_offset; byte altitude_sensor = BARO; // used to know which sensor is active, BARO or SONAR // flight mode specific // -------------------- boolean takeoff_complete; // Flag for using take-off controls boolean land_complete; //int takeoff_altitude; int landing_distance; // meters; long old_alt; // used for managing altitude rates int velocity_land; byte yaw_tracking = MAV_ROI_WPNEXT; // no tracking, point at next wp, or at a target byte brake_timer; // Loiter management // ----------------- long saved_target_bearing; // deg * 100 unsigned long loiter_time; // millis : when we started LOITER mode unsigned long loiter_time_max; // millis : how long to stay in LOITER mode // these are the values for navigation control functions // ---------------------------------------------------- long nav_roll; // deg * 100 : target roll angle long nav_pitch; // deg * 100 : target pitch angle long nav_yaw; // deg * 100 : target yaw angle long nav_lat; // for error calcs long nav_lon; // for error calcs int nav_throttle; // 0-1000 for throttle control int nav_throttle_old; // for filtering long throttle_integrator; // used to control when we calculate nav_throttle bool invalid_throttle; // used to control when we calculate nav_throttle bool invalid_nav; // used to control when we calculate nav_throttle bool set_throttle_cruise_flag = false; // used to track the throttle crouse value long command_yaw_start; // what angle were we to begin with unsigned long command_yaw_start_time; // when did we start turning unsigned int command_yaw_time; // how long we are turning long command_yaw_end; // what angle are we trying to be long command_yaw_delta; // how many degrees will we turn int command_yaw_speed; // how fast to turn byte command_yaw_dir; byte command_yaw_relative; int auto_level_counter; // Waypoints // --------- long wp_distance; // meters - distance between plane and next waypoint long wp_totalDistance; // meters - distance between old and next waypoint byte next_wp_index; // Current active command index // repeating event control // ----------------------- byte event_id; // what to do - see defines unsigned long event_timer; // when the event was asked for in ms unsigned int event_delay; // how long to delay the next firing of event in millis int event_repeat; // how many times to fire : 0 = forever, 1 = do once, 2 = do twice int event_value; // per command value, such as PWM for servos int event_undo_value; // the value used to undo commands byte repeat_forever; byte undo_event; // counter for timing the undo // delay command // -------------- long condition_value; // used in condition commands (eg delay, change alt, etc.) long condition_start; int condition_rate; // land command // ------------ long land_start; // when we intiated command in millis() long original_alt; // altitide reference for start of command // 3D Location vectors // ------------------- struct Location home; // home location struct Location prev_WP; // last waypoint struct Location current_loc; // current location struct Location next_WP; // next waypoint struct Location target_WP; // where do we want to you towards? struct Location simple_WP; // struct Location next_command; // command preloaded long target_altitude; // used for boolean home_is_set; // Flag for if we have g_gps lock and have set the home location // IMU variables // ------------- float G_Dt = 0.02; // Integration time for the gyros (DCM algorithm) // Performance monitoring // ---------------------- long perf_mon_timer; float imu_health; // Metric based on accel gain deweighting int G_Dt_max; // Max main loop cycle time in milliseconds int gps_fix_count; byte gcs_messages_sent; // GCS // --- char GCS_buffer[53]; char display_PID = -1; // Flag used by DebugTerminal to indicate that the next PID calculation with this index should be displayed // System Timers // -------------- unsigned long fast_loopTimer; // Time in miliseconds of main control loop unsigned long fast_loopTimeStamp; // Time Stamp when fast loop was complete uint8_t delta_ms_fast_loop; // Delta Time in miliseconds int mainLoop_count; unsigned long medium_loopTimer; // Time in miliseconds of navigation control loop byte medium_loopCounter; // Counters for branching from main control loop to slower loops uint8_t delta_ms_medium_loop; unsigned long fiftyhz_loopTimer; uint8_t delta_ms_fiftyhz; byte slow_loopCounter; int superslow_loopCounter; byte flight_timer; // for limiting the execution of flight mode thingys unsigned long dTnav; // Delta Time in milliseconds for navigation computations unsigned long nav_loopTimer; // used to track the elapsed ime for GPS nav unsigned long elapsedTime; // for doing custom events float load; // % MCU cycles used byte counter_one_herz; bool GPS_enabled = false; byte loop_step; //////////////////////////////////////////////////////////////////////////////// // Top-level logic //////////////////////////////////////////////////////////////////////////////// void setup() { init_ardupilot(); } void loop() { // We want this to execute fast // ---------------------------- if (millis() - fast_loopTimer >= 5) { delta_ms_fast_loop = millis() - fast_loopTimer; fast_loopTimer = millis(); load = float(fast_loopTimeStamp - fast_loopTimer) / delta_ms_fast_loop; G_Dt = (float)delta_ms_fast_loop / 1000.f; // used by DCM integrator mainLoop_count++; //if (delta_ms_fast_loop > 6) // Log_Write_Performance(); /* if(delta_ms_fast_loop > 11){ update_timer_light(true); //Serial.println(delta_ms_fast_loop,DEC); }else{ update_timer_light(false); }*/ // Execute the fast loop // --------------------- fast_loop(); fast_loopTimeStamp = millis(); } if (millis() - fiftyhz_loopTimer > 19) { delta_ms_fiftyhz = millis() - fiftyhz_loopTimer; fiftyhz_loopTimer = millis(); medium_loop(); fifty_hz_loop(); counter_one_herz++; if(counter_one_herz == 50){ super_slow_loop(); counter_one_herz = 0; } if (millis() - perf_mon_timer > 20000) { if (mainLoop_count != 0) { gcs.send_message(MSG_PERF_REPORT); if (g.log_bitmask & MASK_LOG_PM) Log_Write_Performance(); resetPerfData(); } } } } // Main loop void fast_loop() { // IMU DCM Algorithm read_AHRS(); // This is the fast loop - we want it to execute at >= 100Hz // --------------------------------------------------------- if (delta_ms_fast_loop > G_Dt_max) G_Dt_max = delta_ms_fast_loop; // Read radio // ---------- read_radio(); // read the radio first // custom code/exceptions for flight modes // --------------------------------------- update_current_flight_mode(); // write out the servo PWM values // ------------------------------ set_servos_4(); // record throttle output // ------------------------------ //throttle_integrator += g.rc_3.servo_out; #if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && HIL_MODE != HIL_MODE_DISABLED // HIL for a copter needs very fast update of the servo values hil.send_message(MSG_RADIO_OUT); #endif } void medium_loop() { // reads all of the necessary trig functions for cameras, throttle, etc. update_trig(); // This is the start of the medium (10 Hz) loop pieces // ----------------------------------------- switch(medium_loopCounter) { // This case deals with the GPS and Compass //----------------------------------------- case 0: loop_step = 1; medium_loopCounter++; if(GPS_enabled){ update_GPS(); } //readCommands(); #if HIL_MODE != HIL_MODE_ATTITUDE if(g.compass_enabled){ compass.read(); // Read magnetometer compass.calculate(dcm.get_dcm_matrix()); // Calculate heading //compass.calculate(dcm.roll, dcm.pitch); // Calculate heading compass.null_offsets(dcm.get_dcm_matrix()); } #endif // auto_trim, uses an auto_level algorithm auto_trim(); break; // This case performs some navigation computations //------------------------------------------------ case 1: loop_step = 2; medium_loopCounter++; // hack to stop navigation in Simple mode if (control_mode == SIMPLE){ // clear GPS data g_gps->new_data = false; break; } // Auto control modes: if(g_gps->new_data && g_gps->fix){ loop_step = 11; // invalidate GPS data g_gps->new_data = false; // we are not tracking I term on navigation, so this isn't needed dTnav = millis() - nav_loopTimer; nav_loopTimer = millis(); // calculate the copter's desired bearing and WP distance // ------------------------------------------------------ navigate(); // control mode specific updates to nav_bearing // -------------------------------------------- update_navigation(); if (g.log_bitmask & MASK_LOG_NTUN) Log_Write_Nav_Tuning(); } break; // command processing //------------------- case 2: loop_step = 3; medium_loopCounter++; // Read altitude from sensors // -------------------------- update_alt(); // altitude smoothing // ------------------ //calc_altitude_smoothing_error(); calc_altitude_error(); // invalidate the throttle hold value // ---------------------------------- invalid_throttle = true; break; // This case deals with sending high rate telemetry //------------------------------------------------- case 3: loop_step = 4; medium_loopCounter++; // perform next command // -------------------- if(control_mode == AUTO){ //if(home_is_set){ update_commands(); //} } #if HIL_MODE != HIL_MODE_ATTITUDE if (g.log_bitmask & MASK_LOG_ATTITUDE_MED) Log_Write_Attitude(); if (g.log_bitmask & MASK_LOG_CTUN) Log_Write_Control_Tuning(); #endif // XXX this should be a "GCS medium loop" interface #if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK gcs.data_stream_send(5,45); // send all requested output streams with rates requested // between 5 and 45 Hz #else gcs.send_message(MSG_ATTITUDE); // Sends attitude data #endif #if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0) hil.data_stream_send(5,45); #endif if (g.log_bitmask & MASK_LOG_MOTORS) Log_Write_Motors(); break; // This case controls the slow loop //--------------------------------- case 4: loop_step = 5; medium_loopCounter = 0; delta_ms_medium_loop = millis() - medium_loopTimer; medium_loopTimer = millis(); if (g.battery_monitoring != 0){ read_battery(); } // Accel trims = hold > 2 seconds // Throttle cruise = switch less than 1 second // -------------------------------------------- read_trim_switch(); // Check for engine arming // ----------------------- arm_motors(); // should we be in DCM Fast recovery? // ---------------------------------- check_DCM(); slow_loop(); break; default: // this is just a catch all // ------------------------ medium_loopCounter = 0; break; } } // stuff that happens at 50 hz // --------------------------- void fifty_hz_loop() { // use Yaw to find our bearing error calc_bearing_error(); // guess how close we are - fixed observer calc //calc_distance_error(); # if HIL_MODE == HIL_MODE_DISABLED if (g.log_bitmask & MASK_LOG_ATTITUDE_FAST) Log_Write_Attitude(); if (g.log_bitmask & MASK_LOG_RAW) Log_Write_Raw(); #endif #if CAMERA_STABILIZER == ENABLED camera_stabilization(); #endif // XXX is it appropriate to be doing the comms below on the fast loop? #if HIL_MODE != HIL_MODE_DISABLED && HIL_PORT != GCS_PORT // kick the HIL to process incoming sensor packets hil.update(); #if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK hil.data_stream_send(45,1000); #else hil.send_message(MSG_SERVO_OUT); #endif #elif HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && HIL_MODE == HIL_MODE_DISABLED && HIL_PORT == 0 // Case for hil object on port 0 just for mission planning hil.update(); hil.data_stream_send(45,1000); #endif // kick the GCS to process uplink data gcs.update(); #if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK gcs.data_stream_send(45,1000); #endif // XXX this should be absorbed into the above, // or be a "GCS fast loop" interface #if FRAME_CONFIG == TRI_FRAME // Hack - had to move to 50hz loop to test a theory // servo Yaw g.rc_4.calc_pwm(); APM_RC.OutputCh(CH_7, g.rc_4.radio_out); #endif } void slow_loop() { // This is the slow (3 1/3 Hz) loop pieces //---------------------------------------- switch (slow_loopCounter){ case 0: loop_step = 6; slow_loopCounter++; superslow_loopCounter++; if(superslow_loopCounter > 800){ // every 4 minutes #if HIL_MODE != HIL_MODE_ATTITUDE if(g.rc_3.control_in == 0 && g.compass_enabled){ compass.save_offsets(); superslow_loopCounter = 0; } #endif } break; case 1: loop_step = 7; slow_loopCounter++; // Read 3-position switch on radio // ------------------------------- read_control_switch(); // Read main battery voltage if hooked up - does not read the 5v from radio // ------------------------------------------------------------------------ #if BATTERY_EVENT == 1 read_battery(); #endif #if AUTO_RESET_LOITER == 1 if(control_mode == LOITER){ if((abs(g.rc_2.control_in) + abs(g.rc_1.control_in)) > 500){ // reset LOITER to current position long temp = next_WP.alt; next_WP = current_loc; next_WP.alt = temp; } } #endif break; case 2: loop_step = 8; slow_loopCounter = 0; update_events(); // blink if we are armed update_lights(); // XXX this should be a "GCS slow loop" interface #if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK gcs.data_stream_send(1,5); // send all requested output streams with rates requested // between 1 and 5 Hz #else gcs.send_message(MSG_LOCATION); gcs.send_message(MSG_CPU_LOAD, load*100); #endif #if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0) hil.data_stream_send(1,5); #endif #if CHANNEL_6_TUNING != CH6_NONE tuning(); #endif // filter out the baro offset. //if(baro_alt_offset > 0) baro_alt_offset--; //if(baro_alt_offset < 0) baro_alt_offset++; #if MOTOR_LEDS == 1 update_motor_leds(); #endif break; default: slow_loopCounter = 0; break; } } // 1Hz loop void super_slow_loop() { loop_step = 9; if (g.log_bitmask & MASK_LOG_CURRENT) Log_Write_Current(); gcs.send_message(MSG_HEARTBEAT); // XXX This is running at 3 1/3 Hz instead of 1 Hz #if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0) hil.send_message(MSG_HEARTBEAT); #endif //if(gcs_simple.read()){ // Serial.print("!"); /* Location temp; temp.id = gcs_simple.id; temp.p1 = gcs_simple.p1; temp.alt = gcs_simple.altitude; temp.lat = gcs_simple.latitude; temp.lng = gcs_simple.longitude; set_command_with_index(temp, gcs_simple.index); gcs_simple.ack(); */ //} } void update_GPS(void) { loop_step = 10; g_gps->update(); update_GPS_light(); //current_loc.lng = 377697000; // Lon * 10 * *7 //current_loc.lat = -1224318000; // Lat * 10 * *7 //current_loc.alt = 100; // alt * 10 * *7 //return; if (g_gps->new_data && g_gps->fix) { // XXX We should be sending GPS data off one of the regular loops so that we send // no-GPS-fix data too #if GCS_PROTOCOL != GCS_PROTOCOL_MAVLINK gcs.send_message(MSG_LOCATION); #endif // for performance // --------------- gps_fix_count++; if(ground_start_count > 1){ ground_start_count--; } else if (ground_start_count == 1) { // We countdown N number of good GPS fixes // so that the altitude is more accurate // ------------------------------------- if (current_loc.lat == 0) { SendDebugln("!! bad loc"); ground_start_count = 5; }else{ //Serial.printf("init Home!"); // reset our nav loop timer //nav_loopTimer = millis(); init_home(); // init altitude current_loc.alt = home.alt; ground_start_count = 0; } } current_loc.lng = g_gps->longitude; // Lon * 10 * *7 current_loc.lat = g_gps->latitude; // Lat * 10 * *7 if (g.log_bitmask & MASK_LOG_GPS){ Log_Write_GPS(); } } } void update_current_flight_mode(void) { if(control_mode == AUTO){ // this is a hack to prevent run up of the throttle I term for alt hold if(command_must_ID == MAV_CMD_NAV_TAKEOFF){ invalid_throttle = (g.rc_3.control_in != 0); // make invalid_throttle false if we are waiting to take off. } switch(command_must_ID){ default: // Output Pitch, Roll, Yaw and Throttle // ------------------------------------ auto_yaw(); // mix in user control control_nav_mixer(); // perform stabilzation output_stabilize_roll(); output_stabilize_pitch(); if(invalid_throttle) calc_nav_throttle(); // apply throttle control output_auto_throttle(); break; } }else{ switch(control_mode){ case ACRO: // clear any AP naviagtion values nav_pitch = 0; nav_roll = 0; // Yaw control output_manual_yaw(); // apply throttle control output_manual_throttle(); // mix in user control control_nav_mixer(); // perform rate or stabilzation // ---------------------------- // Roll control if(abs(g.rc_1.control_in) >= ACRO_RATE_TRIGGER){ output_rate_roll(); // rate control yaw }else{ output_stabilize_roll(); // hold yaw } // Roll control if(abs(g.rc_2.control_in) >= ACRO_RATE_TRIGGER){ output_rate_pitch(); // rate control yaw }else{ output_stabilize_pitch(); // hold yaw } break; case STABILIZE: // clear any AP naviagtion values nav_pitch = 0; nav_roll = 0; if(g.rc_3.control_in == 0){ clear_yaw_control(); }else{ // Yaw control output_manual_yaw(); } // apply throttle control output_manual_throttle(); // mix in user control control_nav_mixer(); // perform stabilzation output_stabilize_roll(); output_stabilize_pitch(); break; case SIMPLE: flight_timer++; // 25 hz if(flight_timer > 4){ flight_timer = 0; simple_WP.lat = 0; simple_WP.lng = 0; next_WP.lng = (float)g.rc_1.control_in *.4; // X: 4500 / 2 = 2250 = 25 meteres next_WP.lat = -((float)g.rc_2.control_in *.4); // Y: 4500 / 2 = 2250 = 25 meteres // calc a new bearing nav_bearing = get_bearing(&simple_WP, &next_WP) + initial_simple_bearing; nav_bearing = wrap_360(nav_bearing); wp_distance = get_distance(&simple_WP, &next_WP); calc_bearing_error(); /* Serial.printf("lat: %ld lon:%ld, bear:%ld, dist:%ld, init:%ld, err:%ld ", next_WP.lat, next_WP.lng, nav_bearing, wp_distance, initial_simple_bearing, bearing_error); */ // get nav_pitch and nav_roll calc_simple_nav(); calc_nav_output(); limit_nav_pitch_roll(4500); } // are we at rest? reset nav_yaw if(g.rc_3.control_in == 0){ clear_yaw_control(); }else{ // Yaw control output_manual_yaw(); } // apply throttle control output_manual_throttle(); // apply nav_pitch and nav_roll to output simple_mixer(); // perform stabilzation output_stabilize_roll(); output_stabilize_pitch(); break; case ALT_HOLD: // clear any AP naviagtion values nav_pitch = 0; nav_roll = 0; // allow interactive changing of atitude adjust_altitude(); // Yaw control // ----------- output_manual_yaw(); // Output Pitch, Roll, Yaw and Throttle // ------------------------------------ if(invalid_throttle) calc_nav_throttle(); // apply throttle control output_auto_throttle(); // mix in user control control_nav_mixer(); // perform stabilzation output_stabilize_roll(); output_stabilize_pitch(); break; case RTL: // Output Pitch, Roll, Yaw and Throttle // ------------------------------------ auto_yaw(); if(invalid_throttle) calc_nav_throttle(); // apply throttle control output_auto_throttle(); // mix in user control with Nav control control_nav_mixer(); // perform stabilzation output_stabilize_roll(); output_stabilize_pitch(); break; case LOITER: // allow interactive changing of atitude adjust_altitude(); // Output Pitch, Roll, Yaw and Throttle // ------------------------------------ // Yaw control // ----------- output_manual_yaw(); if(invalid_throttle) calc_nav_throttle(); // apply throttle control output_auto_throttle(); // mix in user control with Nav control control_nav_mixer(); // perform stabilzation output_stabilize_roll(); output_stabilize_pitch(); break; default: //Serial.print("$"); break; } } } // called after a GPS read void update_navigation() { // wp_distance is in ACTUAL meters, not the *100 meters we get from the GPS // ------------------------------------------------------------------------ switch(control_mode){ case AUTO: verify_commands(); // note: wp_control is handled by commands_logic // calculates desired Yaw update_nav_yaw(); // calculates the desired Roll and Pitch update_nav_wp(); break; case RTL: // calculates desired Yaw update_nav_yaw(); case LOITER: // are we Traversing or Loitering? wp_control = (wp_distance < 50) ? LOITER_MODE : WP_MODE; //wp_control = LOITER_MODE; // calculates the desired Roll and Pitch update_nav_wp(); break; /*#if YAW_HACK == 1 case SIMPLE: // calculates desired Yaw // exprimental_hack if(g.rc_6.control_in > 900) update_nav_yaw(); if(g.rc_6.control_in < 100){ nav_yaw = dcm.yaw_sensor; } break; #endif */ } } void read_AHRS(void) { // Perform IMU calculations and get attitude info //----------------------------------------------- #if HIL_MODE == HIL_MODE_SENSORS // update hil before dcm update hil.update(); #endif dcm.update_DCM(G_Dt); omega = dcm.get_gyro(); } void update_trig(void){ Vector2f yawvector; Matrix3f temp = dcm.get_dcm_matrix(); yawvector.x = temp.a.x; // sin yawvector.y = temp.b.x; // cos yawvector.normalize(); cos_yaw_x = yawvector.y; // 0 x = north sin_yaw_y = yawvector.x; // 1 y sin_pitch_y = -temp.c.x; cos_pitch_x = sqrt(1 - (temp.c.x * temp.c.x)); cos_roll_x = temp.c.z / cos_pitch_x; sin_roll_y = temp.c.y / cos_pitch_x; } // updated at 10hz void update_alt() { altitude_sensor = BARO; #if HIL_MODE == HIL_MODE_ATTITUDE current_loc.alt = g_gps->altitude; #else if(g.sonar_enabled){ // filter out offset float scale; // read barometer baro_alt = read_barometer(); int temp_sonar = sonar.read(); // spike filter //if((temp_sonar - sonar_alt) < 50){ sonar_alt = temp_sonar; //} scale = (sonar_alt - 300) / 300; scale = constrain(scale, 0, 1); current_loc.alt = ((float)sonar_alt * (1.0 - scale)) + ((float)baro_alt * scale) + home.alt; }else{ baro_alt = read_barometer(); // no sonar altitude current_loc.alt = baro_alt + home.alt; } #endif } // updated at 10hz void update_alt2() { altitude_sensor = BARO; #if HIL_MODE == HIL_MODE_ATTITUDE current_loc.alt = g_gps->altitude; #else if(g.sonar_enabled){ // filter out offset // read barometer baro_alt = read_barometer(); int temp_sonar = sonar.read(); // spike filter if((temp_sonar - sonar_alt) < 50){ sonar_alt = temp_sonar; } // decide if we're using sonar if ((baro_alt < 1200) || sonar_alt < 300){ // correct alt for angle of the sonar float temp = cos_pitch_x * cos_roll_x; temp = max(temp, 0.707); sonar_alt = (float)sonar_alt * temp; if(sonar_alt < 450){ altitude_sensor = SONAR; baro_alt_offset = sonar_alt - baro_alt; } } // calculate our altitude if(altitude_sensor == BARO){ current_loc.alt = baro_alt + baro_alt_offset + home.alt; }else{ current_loc.alt = sonar_alt + home.alt; } }else{ baro_alt = read_barometer(); // no sonar altitude current_loc.alt = baro_alt + home.alt; } //Serial.printf("b_alt: %ld, home: %ld ", baro_alt, home.alt); #endif } void adjust_altitude() { flight_timer++; if(flight_timer >= 2){ flight_timer = 0; if(g.rc_3.control_in <= 200){ next_WP.alt -= 1; // 1 meter per second next_WP.alt = max(next_WP.alt, (current_loc.alt - 100)); // don't go more than 4 meters below current location next_WP.alt = max(next_WP.alt, 100); // no lower than 1 meter? }else if (g.rc_3.control_in > 700){ next_WP.alt += 2; // 1 meter per second //next_WP.alt = min((current_loc.alt + 400), next_WP.alt); // don't go more than 4 meters below current location next_WP.alt = min(next_WP.alt, (current_loc.alt + 200)); // don't go more than 4 meters below current location } } } void tuning(){ #if CHANNEL_6_TUNING == CH6_STABLIZE_KP g.pid_stabilize_roll.kP((float)g.rc_6.control_in / 1000.0); g.pid_stabilize_pitch.kP((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_STABLIZE_KD // uncomment me out to try in flight dampening, 0 = unflyable, .2 = unfun, .13 worked for me. // use test,radio to get the value to use in your config. g.pid_stabilize_pitch.kD((float)g.rc_6.control_in / 1000.0); g.pid_stabilize_roll.kD((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_BARO_KP g.pid_baro_throttle.kP((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_BARO_KD g.pid_baro_throttle.kD((float)g.rc_6.control_in / 1000.0); // 0 to 1 #elif CHANNEL_6_TUNING == CH6_SONAR_KP g.pid_sonar_throttle.kP((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_SONAR_KD g.pid_sonar_throttle.kD((float)g.rc_6.control_in / 1000.0); // 0 to 1 #elif CHANNEL_6_TUNING == CH6_Y6_SCALING Y6_scaling = (float)g.rc_6.control_in / 1000.0; #elif CHANNEL_6_TUNING == CH6_PMAX g.pitch_max.set(g.rc_6.control_in * 2); // 0 to 2000 #elif CHANNEL_6_TUNING == CH6_DCM_RP dcm.kp_roll_pitch((float)g.rc_6.control_in / 5000.0); #elif CHANNEL_6_TUNING == CH6_DCM_Y dcm.kp_yaw((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_YAW_KP // yaw heading g.pid_yaw.kP((float)g.rc_6.control_in / 200.0); // range from 0.0 ~ 5.0 #elif CHANNEL_6_TUNING == CH6_YAW_KD // yaw heading g.pid_yaw.kD((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_YAW_RATE_KP // yaw rate g.pid_acro_rate_yaw.kP((float)g.rc_6.control_in / 1000.0); #elif CHANNEL_6_TUNING == CH6_YAW_RATE_KD // yaw rate g.pid_acro_rate_yaw.kD((float)g.rc_6.control_in / 1000.0); #endif } void update_nav_wp() { if(wp_control == LOITER_MODE){ // calc a pitch to the target calc_loiter_nav(); // rotate pitch and roll to the copter frame of reference calc_loiter_output(); } else { // how far are we from the ideal trajectory? // this pushes us back on course update_crosstrack(); // calc a rate dampened pitch to the target calc_rate_nav(); // rotate that pitch to the copter frame of reference calc_nav_output(); } } void update_nav_yaw() { // this tracks a location so the copter is always pointing towards it. if(yaw_tracking == MAV_ROI_LOCATION){ nav_yaw = get_bearing(¤t_loc, &target_WP); }else if(yaw_tracking == MAV_ROI_WPNEXT){ nav_yaw = target_bearing; } } void check_DCM() { #if DYNAMIC_DRIFT == 1 if(g.rc_1.control_in == 0 && g.rc_2.control_in == 0){ if(g.rc_3.control_in < (g.throttle_cruise + 20)){ //dcm.kp_roll_pitch(dcm.kDCM_kp_rp_high); dcm.kp_roll_pitch(0.15); } }else{ dcm.kp_roll_pitch(0.05967); } #endif }