// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /***************************************************************************** The init_ardupilot function processes everything we need for an in - air restart We will determine later if we are actually on the ground and process a ground start in that case. *****************************************************************************/ #if CLI_ENABLED == ENABLED // Functions called from the top-level menu static int8_t process_logs(uint8_t argc, const Menu::arg *argv); // in Log.pde static int8_t setup_mode(uint8_t argc, const Menu::arg *argv); // in setup.pde static int8_t test_mode(uint8_t argc, const Menu::arg *argv); // in test.cpp static int8_t planner_mode(uint8_t argc, const Menu::arg *argv); // in planner.pde // This is the help function // PSTR is an AVR macro to read strings from flash memory // printf_P is a version of print_f that reads from flash memory static int8_t main_menu_help(uint8_t argc, const Menu::arg *argv) { Serial.printf_P(PSTR("Commands:\n" " logs\n" " setup\n" " test\n" " planner\n" "\n" "Move the slide switch and reset to FLY.\n" "\n")); return(0); } // Command/function table for the top-level menu. const struct Menu::command main_menu_commands[] PROGMEM = { // command function called // ======= =============== {"logs", process_logs}, {"setup", setup_mode}, {"test", test_mode}, {"help", main_menu_help}, {"planner", planner_mode} }; // Create the top-level menu object. MENU(main_menu, THISFIRMWARE, main_menu_commands); // the user wants the CLI. It never exits static void run_cli(void) { while (1) { main_menu.run(); } } #endif // CLI_ENABLED static void init_ardupilot() { #if USB_MUX_PIN > 0 // on the APM2 board we have a mux thet switches UART0 between // USB and the board header. If the right ArduPPM firmware is // installed we can detect if USB is connected using the // USB_MUX_PIN pinMode(USB_MUX_PIN, INPUT); usb_connected = !digitalRead(USB_MUX_PIN); if (!usb_connected) { // USB is not connected, this means UART0 may be a Xbee, with // its darned bricking problem. We can't write to it for at // least one second after powering up. Simplest solution for // now is to delay for 1 second. Something more elegant may be // added later delay(1000); } #endif // Console serial port // // The console port buffers are defined to be sufficiently large to support // the MAVLink protocol efficiently // Serial.begin(SERIAL0_BAUD, 128, 256); // GPS serial port. // #if GPS_PROTOCOL != GPS_PROTOCOL_IMU Serial1.begin(38400, 128, 16); #endif Serial.printf_P(PSTR("\n\nInit " THISFIRMWARE "\n\nFree RAM: %u\n"), memcheck_available_memory()); // // Initialize Wire and SPI libraries // #ifndef DESKTOP_BUILD I2c.begin(); I2c.timeOut(5); // initially set a fast I2c speed, and drop it on first failures I2c.setSpeed(true); #endif SPI.begin(); SPI.setClockDivider(SPI_CLOCK_DIV16); // 1MHZ SPI rate // // Initialize the isr_registry. // isr_registry.init(); // // Check the EEPROM format version before loading any parameters from EEPROM. // report_version(); // setup IO pins pinMode(A_LED_PIN, OUTPUT); // GPS status LED digitalWrite(A_LED_PIN, LED_OFF); pinMode(B_LED_PIN, OUTPUT); // GPS status LED digitalWrite(B_LED_PIN, LED_OFF); pinMode(C_LED_PIN, OUTPUT); // GPS status LED digitalWrite(C_LED_PIN, LED_OFF); #if SLIDE_SWITCH_PIN > 0 pinMode(SLIDE_SWITCH_PIN, INPUT); // To enter interactive mode #endif #if CONFIG_PUSHBUTTON == ENABLED pinMode(PUSHBUTTON_PIN, INPUT); // unused #endif #if CONFIG_RELAY == ENABLED DDRL |= B00000100; // Set Port L, pin 2 to output for the relay #endif #if COPTER_LEDS == ENABLED pinMode(COPTER_LED_1, OUTPUT); //Motor LED pinMode(COPTER_LED_2, OUTPUT); //Motor LED pinMode(COPTER_LED_3, OUTPUT); //Motor LED pinMode(COPTER_LED_4, OUTPUT); //Motor LED pinMode(COPTER_LED_5, OUTPUT); //Motor or Aux LED pinMode(COPTER_LED_6, OUTPUT); //Motor or Aux LED pinMode(COPTER_LED_7, OUTPUT); //Motor or GPS LED pinMode(COPTER_LED_8, OUTPUT); //Motor or GPS LED #endif #if PIEZO == 1 pinMode(PIEZO_PIN,OUTPUT); piezo_beep(); #endif // load parameters from EEPROM load_parameters(); // init the GCS gcs0.init(&Serial); #if USB_MUX_PIN > 0 if (!usb_connected) { // we are not connected via USB, re-init UART0 with right // baud rate Serial.begin(map_baudrate(g.serial3_baud, SERIAL3_BAUD)); } #else // we have a 2nd serial port for telemetry Serial3.begin(map_baudrate(g.serial3_baud, SERIAL3_BAUD), 128, 256); gcs3.init(&Serial3); #endif // identify ourselves correctly with the ground station mavlink_system.sysid = g.sysid_this_mav; mavlink_system.type = 2; //MAV_QUADROTOR; #if LOGGING_ENABLED == ENABLED DataFlash.Init(); if (!DataFlash.CardInserted()) { gcs_send_text_P(SEVERITY_LOW, PSTR("No dataflash inserted")); g.log_bitmask.set(0); } else if (DataFlash.NeedErase()) { gcs_send_text_P(SEVERITY_LOW, PSTR("ERASING LOGS")); do_erase_logs(); } if (g.log_bitmask != 0){ DataFlash.start_new_log(); } #endif #ifdef RADIO_OVERRIDE_DEFAULTS { int16_t rc_override[8] = RADIO_OVERRIDE_DEFAULTS; APM_RC.setHIL(rc_override); } #endif #if FRAME_CONFIG == HELI_FRAME motors.servo_manual = false; motors.init_swash(); // heli initialisation #endif RC_Channel::set_apm_rc(&APM_RC); init_rc_in(); // sets up rc channels from radio init_rc_out(); // sets up the timer libs init_camera(); timer_scheduler.init( &isr_registry ); #if HIL_MODE != HIL_MODE_ATTITUDE #if CONFIG_ADC == ENABLED // begin filtering the ADC Gyros adc.Init(&timer_scheduler); // APM ADC library initialization #endif // CONFIG_ADC barometer.init(&timer_scheduler); #endif // HIL_MODE // Do GPS init g_gps = &g_gps_driver; g_gps->init(); // GPS Initialization g_gps->callback = mavlink_delay; if(g.compass_enabled) init_compass(); // init the optical flow sensor if(g.optflow_enabled) { init_optflow(); } // agmatthews USERHOOKS #ifdef USERHOOK_INIT USERHOOK_INIT #endif #if CLI_ENABLED == ENABLED && CLI_SLIDER_ENABLED == ENABLED // If the switch is in 'menu' mode, run the main menu. // // Since we can't be sure that the setup or test mode won't leave // the system in an odd state, we don't let the user exit the top // menu; they must reset in order to fly. // if (check_startup_for_CLI()) { digitalWrite(A_LED_PIN, LED_ON); // turn on setup-mode LED Serial.printf_P(PSTR("\nCLI:\n\n")); run_cli(); } #else Serial.printf_P(PSTR("\nPress ENTER 3 times for CLI\n\n")); #endif // CLI_ENABLED GPS_enabled = false; #if HIL_MODE == HIL_MODE_DISABLED // Read in the GPS for (byte counter = 0; ; counter++) { g_gps->update(); if (g_gps->status() != 0){ GPS_enabled = true; break; } if (counter >= 2) { GPS_enabled = false; break; } } #else GPS_enabled = true; #endif // lengthen the idle timeout for gps Auto_detect // --------------------------------------------- g_gps->idleTimeout = 20000; // print the GPS status // -------------------- report_gps(); #if HIL_MODE != HIL_MODE_ATTITUDE // read Baro pressure at ground //----------------------------- init_barometer(); #endif // initialise sonar #if CONFIG_SONAR == ENABLED init_sonar(); #endif // initialize commands // ------------------- init_commands(); // set the correct flight mode // --------------------------- reset_control_switch(); // init the Z damopener // -------------------- #if ACCEL_ALT_HOLD != 0 init_z_damper(); #endif startup_ground(); #if LOGGING_ENABLED == ENABLED Log_Write_Startup(); Log_Write_Data(10, (float)g.pi_stabilize_roll.kP()); Log_Write_Data(11, (float)g.pi_stabilize_roll.kI()); Log_Write_Data(12, (float)g.pid_rate_roll.kP()); Log_Write_Data(13, (float)g.pid_rate_roll.kI()); Log_Write_Data(14, (float)g.pid_rate_roll.kD()); Log_Write_Data(15, (float)g.stabilize_d.get()); Log_Write_Data(16, (float)g.pi_loiter_lon.kP()); Log_Write_Data(17, (float)g.pi_loiter_lon.kI()); Log_Write_Data(18, (float)g.pid_nav_lon.kP()); Log_Write_Data(19, (float)g.pid_nav_lon.kI()); Log_Write_Data(20, (float)g.pid_nav_lon.kD()); Log_Write_Data(21, (int32_t)g.auto_slew_rate.get()); Log_Write_Data(22, (float)g.pid_loiter_rate_lon.kP()); Log_Write_Data(23, (float)g.pid_loiter_rate_lon.kI()); Log_Write_Data(24, (float)g.pid_loiter_rate_lon.kD()); #endif SendDebug("\nReady to FLY "); } //******************************************************************************** //This function does all the calibrations, etc. that we need during a ground start //******************************************************************************** static void startup_ground(void) { gcs_send_text_P(SEVERITY_LOW,PSTR("GROUND START")); #if HIL_MODE != HIL_MODE_ATTITUDE // Warm up and read Gyro offsets // ----------------------------- imu.init(IMU::COLD_START, mavlink_delay, flash_leds, &timer_scheduler); #if CLI_ENABLED == ENABLED report_imu(); #endif #endif // reset the leds // --------------------------- clear_leds(); // when we re-calibrate the gyros, // all previous I values are invalid reset_I_all(); } /* #define YAW_HOLD 0 #define YAW_ACRO 1 #define YAW_AUTO 2 #define YAW_LOOK_AT_HOME 3 #define ROLL_PITCH_STABLE 0 #define ROLL_PITCH_ACRO 1 #define ROLL_PITCH_AUTO 2 #define THROTTLE_MANUAL 0 #define THROTTLE_HOLD 1 #define THROTTLE_AUTO 2 */ static void set_mode(byte mode) { // if we don't have GPS lock if(home_is_set == false){ // our max mode should be if (mode > ALT_HOLD && mode != OF_LOITER) mode = STABILIZE; } // nothing but OF_LOITER for OptFlow only if (g.optflow_enabled && GPS_enabled == false){ if (mode > ALT_HOLD && mode != OF_LOITER) mode = STABILIZE; } old_control_mode = control_mode; control_mode = mode; control_mode = constrain(control_mode, 0, NUM_MODES - 1); // used to stop fly_aways motors.auto_armed(g.rc_3.control_in > 0); // clearing value used in interactive alt hold manual_boost = 0; // clearing value used to force the copter down in landing mode landing_boost = 0; // do we want to come to a stop or pass a WP? slow_wp = false; // do not auto_land if we are leaving RTL loiter_timer = 0; // if we change modes, we must clear landed flag land_complete = false; // debug to Serial terminal //Serial.println(flight_mode_strings[control_mode]); // report the GPS and Motor arming status led_mode = NORMAL_LEDS; switch(control_mode) { case ACRO: yaw_mode = YAW_HOLD; roll_pitch_mode = ROLL_PITCH_ACRO; throttle_mode = THROTTLE_MANUAL; break; case STABILIZE: yaw_mode = YAW_HOLD; roll_pitch_mode = ROLL_PITCH_STABLE; throttle_mode = THROTTLE_MANUAL; break; case ALT_HOLD: yaw_mode = ALT_HOLD_YAW; roll_pitch_mode = ALT_HOLD_RP; throttle_mode = ALT_HOLD_THR; force_new_altitude(max(current_loc.alt, 100)); break; case AUTO: yaw_mode = AUTO_YAW; roll_pitch_mode = AUTO_RP; throttle_mode = AUTO_THR; // loads the commands from where we left off init_commands(); break; case CIRCLE: yaw_mode = CIRCLE_YAW; roll_pitch_mode = CIRCLE_RP; throttle_mode = CIRCLE_THR; set_next_WP(¤t_loc); circle_angle = 0; break; case LOITER: yaw_mode = LOITER_YAW; roll_pitch_mode = LOITER_RP; throttle_mode = LOITER_THR; set_next_WP(¤t_loc); break; case POSITION: yaw_mode = YAW_HOLD; roll_pitch_mode = ROLL_PITCH_AUTO; throttle_mode = THROTTLE_MANUAL; set_next_WP(¤t_loc); break; case GUIDED: yaw_mode = YAW_AUTO; roll_pitch_mode = ROLL_PITCH_AUTO; throttle_mode = THROTTLE_AUTO; next_WP = current_loc; set_next_WP(&guided_WP); break; case LAND: yaw_mode = LOITER_YAW; roll_pitch_mode = LOITER_RP; throttle_mode = THROTTLE_AUTO; do_land(); break; case APPROACH: yaw_mode = LOITER_YAW; roll_pitch_mode = LOITER_RP; throttle_mode = THROTTLE_AUTO; do_approach(); break; case RTL: yaw_mode = RTL_YAW; roll_pitch_mode = RTL_RP; throttle_mode = RTL_THR; do_RTL(); break; case OF_LOITER: yaw_mode = OF_LOITER_YAW; roll_pitch_mode = OF_LOITER_RP; throttle_mode = OF_LOITER_THR; set_next_WP(¤t_loc); break; default: break; } if(failsafe){ // this is to allow us to fly home without interactive throttle control throttle_mode = THROTTLE_AUTO; // does not wait for us to be in high throttle, since the // Receiver will be outputting low throttle motors.auto_armed(true); } // called to calculate gain for alt hold update_throttle_cruise(); if(roll_pitch_mode <= ROLL_PITCH_ACRO){ // We are under manual attitude control // remove the navigation from roll and pitch command reset_nav_params(); // remove the wind compenstaion reset_wind_I(); // Clears the alt hold compensation reset_throttle_I(); } Log_Write_Mode(control_mode); } static void set_failsafe(boolean mode) { // only act on changes // ------------------- if(failsafe != mode){ // store the value so we don't trip the gate twice // ----------------------------------------------- failsafe = mode; if (failsafe == false){ // We've regained radio contact // ---------------------------- failsafe_off_event(); }else{ // We've lost radio contact // ------------------------ failsafe_on_event(); } } } static void init_simple_bearing() { initial_simple_bearing = ahrs.yaw_sensor; } static void update_throttle_cruise() { int16_t tmp = g.pi_alt_hold.get_integrator(); if(tmp != 0){ g.throttle_cruise += tmp; reset_throttle_I(); } // recalc kp //g.pid_throttle.kP((float)g.throttle_cruise.get() / 981.0); //Serial.printf("kp:%1.4f\n",kp); } #if CLI_SLIDER_ENABLED == ENABLED && CLI_ENABLED == ENABLED static boolean check_startup_for_CLI() { return (digitalRead(SLIDE_SWITCH_PIN) == 0); } #endif // CLI_ENABLED /* map from a 8 bit EEPROM baud rate to a real baud rate */ static uint32_t map_baudrate(int8_t rate, uint32_t default_baud) { switch (rate) { case 1: return 1200; case 2: return 2400; case 4: return 4800; case 9: return 9600; case 19: return 19200; case 38: return 38400; case 57: return 57600; case 111: return 111100; case 115: return 115200; } //Serial.println_P(PSTR("Invalid SERIAL3_BAUD")); return default_baud; } #if USB_MUX_PIN > 0 static void check_usb_mux(void) { bool usb_check = !digitalRead(USB_MUX_PIN); if (usb_check == usb_connected) { return; } // the user has switched to/from the telemetry port usb_connected = usb_check; if (usb_connected) { Serial.begin(SERIAL0_BAUD); } else { Serial.begin(map_baudrate(g.serial3_baud, SERIAL3_BAUD)); } } #endif /* called by gyro/accel init to flash LEDs so user has some mesmerising lights to watch while waiting */ void flash_leds(bool on) { digitalWrite(A_LED_PIN, on?LED_OFF:LED_ON); digitalWrite(C_LED_PIN, on?LED_ON:LED_OFF); } #ifndef DESKTOP_BUILD /* * Read Vcc vs 1.1v internal reference * * This call takes about 150us total. ADC conversion is 13 cycles of * 125khz default changes the mux if it isn't set, and return last * reading (allows necessary settle time) otherwise trigger the * conversion */ uint16_t board_voltage(void) { const uint8_t mux = (_BV(REFS0)|_BV(MUX4)|_BV(MUX3)|_BV(MUX2)|_BV(MUX1)); if (ADMUX == mux) { ADCSRA |= _BV(ADSC); // Convert uint16_t counter=4000; // normally takes about 1700 loops while (bit_is_set(ADCSRA, ADSC) && counter) // Wait counter--; if (counter == 0) { // we don't actually expect this timeout to happen, // but we don't want any more code that could hang. We // report 0V so it is clear in the logs that we don't know // the value return 0; } uint32_t result = ADCL | ADCH<<8; return 1126400UL / result; // Read and back-calculate Vcc in mV } // switch mux, settle time is needed. We don't want to delay // waiting for the settle, so report 0 as a "don't know" value ADMUX = mux; return 0; // we don't know the current voltage } #endif