mirror of https://github.com/ArduPilot/ardupilot
453 lines
12 KiB
C++
453 lines
12 KiB
C++
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#include "Copter.h"
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/*****************************************************************************
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* The init_ardupilot function processes everything we need for an in - air restart
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* We will determine later if we are actually on the ground and process a
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* ground start in that case.
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*
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*****************************************************************************/
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#if CLI_ENABLED == ENABLED
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// This is the help function
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int8_t Copter::main_menu_help(uint8_t argc, const Menu::arg *argv)
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{
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cliSerial->printf("Commands:\n"
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" logs\n"
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" setup\n"
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" test\n"
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" reboot\n"
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"\n");
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return(0);
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}
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// Command/function table for the top-level menu.
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const struct Menu::command main_menu_commands[] = {
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// command function called
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// ======= ===============
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{"logs", MENU_FUNC(process_logs)},
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{"setup", MENU_FUNC(setup_mode)},
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{"test", MENU_FUNC(test_mode)},
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{"reboot", MENU_FUNC(reboot_board)},
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{"help", MENU_FUNC(main_menu_help)},
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};
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// Create the top-level menu object.
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MENU(main_menu, THISFIRMWARE, main_menu_commands);
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int8_t Copter::reboot_board(uint8_t argc, const Menu::arg *argv)
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{
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hal.scheduler->reboot(false);
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return 0;
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}
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// the user wants the CLI. It never exits
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void Copter::run_cli(AP_HAL::UARTDriver *port)
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{
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cliSerial = port;
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Menu::set_port(port);
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port->set_blocking_writes(true);
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// disable the mavlink delay callback
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hal.scheduler->register_delay_callback(NULL, 5);
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// disable main_loop failsafe
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failsafe_disable();
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// cut the engines
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if(motors.armed()) {
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motors.armed(false);
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motors.output();
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}
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while (1) {
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main_menu.run();
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}
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}
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#endif // CLI_ENABLED
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static void mavlink_delay_cb_static()
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{
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copter.mavlink_delay_cb();
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}
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static void failsafe_check_static()
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{
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copter.failsafe_check();
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}
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void Copter::init_ardupilot()
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{
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if (!hal.gpio->usb_connected()) {
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// USB is not connected, this means UART0 may be a Xbee, with
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// its darned bricking problem. We can't write to it for at
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// least one second after powering up. Simplest solution for
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// now is to delay for 1 second. Something more elegant may be
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// added later
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delay(1000);
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}
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// initialise serial port
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serial_manager.init_console();
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// init vehicle capabilties
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init_capabilities();
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cliSerial->printf("\n\nInit " FIRMWARE_STRING
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"\n\nFree RAM: %u\n",
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(unsigned)hal.util->available_memory());
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//
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// Report firmware version code expect on console (check of actual EEPROM format version is done in load_parameters function)
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//
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report_version();
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// load parameters from EEPROM
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load_parameters();
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BoardConfig.init();
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// initialise serial port
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serial_manager.init();
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// init EPM cargo gripper
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#if EPM_ENABLED == ENABLED
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epm.init();
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#endif
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// initialise notify system
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// disable external leds if epm is enabled because of pin conflict on the APM
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notify.init(true);
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// initialise battery monitor
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battery.init();
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// Init RSSI
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rssi.init();
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barometer.init();
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// Register the mavlink service callback. This will run
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// anytime there are more than 5ms remaining in a call to
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// hal.scheduler->delay.
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hal.scheduler->register_delay_callback(mavlink_delay_cb_static, 5);
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// we start by assuming USB connected, as we initialed the serial
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// port with SERIAL0_BAUD. check_usb_mux() fixes this if need be.
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ap.usb_connected = true;
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check_usb_mux();
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// init the GCS connected to the console
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gcs[0].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_Console, 0);
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// init telemetry port
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gcs[1].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, 0);
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// setup serial port for telem2
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gcs[2].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, 1);
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// setup serial port for fourth telemetry port (not used by default)
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gcs[3].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, 2);
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#if FRSKY_TELEM_ENABLED == ENABLED
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// setup frsky
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frsky_telemetry.init(serial_manager);
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#endif
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// identify ourselves correctly with the ground station
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mavlink_system.sysid = g.sysid_this_mav;
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#if LOGGING_ENABLED == ENABLED
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log_init();
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#endif
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// update motor interlock state
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update_using_interlock();
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#if FRAME_CONFIG == HELI_FRAME
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// trad heli specific initialisation
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heli_init();
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#endif
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init_rc_in(); // sets up rc channels from radio
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init_rc_out(); // sets up motors and output to escs
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// initialise which outputs Servo and Relay events can use
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ServoRelayEvents.set_channel_mask(~motors.get_motor_mask());
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relay.init();
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/*
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* setup the 'main loop is dead' check. Note that this relies on
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* the RC library being initialised.
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*/
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hal.scheduler->register_timer_failsafe(failsafe_check_static, 1000);
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// Do GPS init
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gps.init(&DataFlash, serial_manager);
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if(g.compass_enabled)
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init_compass();
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#if OPTFLOW == ENABLED
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// make optflow available to AHRS
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ahrs.set_optflow(&optflow);
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#endif
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// initialise attitude and position controllers
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attitude_control.set_dt(MAIN_LOOP_SECONDS);
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pos_control.set_dt(MAIN_LOOP_SECONDS);
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// init the optical flow sensor
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init_optflow();
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#if MOUNT == ENABLED
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// initialise camera mount
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camera_mount.init(&DataFlash, serial_manager);
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#endif
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#if PRECISION_LANDING == ENABLED
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// initialise precision landing
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init_precland();
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#endif
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#ifdef USERHOOK_INIT
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USERHOOK_INIT
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#endif
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#if CLI_ENABLED == ENABLED
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if (g.cli_enabled) {
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const char *msg = "\nPress ENTER 3 times to start interactive setup\n";
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cliSerial->println(msg);
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if (gcs[1].initialised && (gcs[1].get_uart() != NULL)) {
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gcs[1].get_uart()->println(msg);
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}
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if (num_gcs > 2 && gcs[2].initialised && (gcs[2].get_uart() != NULL)) {
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gcs[2].get_uart()->println(msg);
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}
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}
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#endif // CLI_ENABLED
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#if HIL_MODE != HIL_MODE_DISABLED
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while (barometer.get_last_update() == 0) {
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// the barometer begins updating when we get the first
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// HIL_STATE message
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gcs_send_text(MAV_SEVERITY_WARNING, "Waiting for first HIL_STATE message");
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delay(1000);
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}
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// set INS to HIL mode
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ins.set_hil_mode();
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#endif
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// read Baro pressure at ground
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//-----------------------------
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init_barometer(true);
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// initialise sonar
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#if CONFIG_SONAR == ENABLED
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init_sonar();
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#endif
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// initialise AP_RPM library
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rpm_sensor.init();
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// initialise mission library
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mission.init();
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// initialise the flight mode and aux switch
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// ---------------------------
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reset_control_switch();
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init_aux_switches();
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startup_INS_ground();
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// set landed flags
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set_land_complete(true);
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set_land_complete_maybe(true);
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// we don't want writes to the serial port to cause us to pause
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// mid-flight, so set the serial ports non-blocking once we are
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// ready to fly
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serial_manager.set_blocking_writes_all(false);
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// enable CPU failsafe
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failsafe_enable();
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ins.set_raw_logging(should_log(MASK_LOG_IMU_RAW));
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ins.set_dataflash(&DataFlash);
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cliSerial->print("\nReady to FLY ");
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// flag that initialisation has completed
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ap.initialised = true;
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}
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//******************************************************************************
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//This function does all the calibrations, etc. that we need during a ground start
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//******************************************************************************
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void Copter::startup_INS_ground()
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{
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// initialise ahrs (may push imu calibration into the mpu6000 if using that device).
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ahrs.init();
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ahrs.set_vehicle_class(AHRS_VEHICLE_COPTER);
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// Warm up and calibrate gyro offsets
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ins.init(scheduler.get_loop_rate_hz());
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// reset ahrs including gyro bias
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ahrs.reset();
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}
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// calibrate gyros - returns true if succesfully calibrated
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bool Copter::calibrate_gyros()
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{
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// gyro offset calibration
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copter.ins.init_gyro();
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// reset ahrs gyro bias
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if (copter.ins.gyro_calibrated_ok_all()) {
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copter.ahrs.reset_gyro_drift();
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return true;
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}
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return false;
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}
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// position_ok - returns true if the horizontal absolute position is ok and home position is set
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bool Copter::position_ok()
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{
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// return false if ekf failsafe has triggered
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if (failsafe.ekf) {
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return false;
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}
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// check ekf position estimate
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return (ekf_position_ok() || optflow_position_ok());
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}
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// ekf_position_ok - returns true if the ekf claims it's horizontal absolute position estimate is ok and home position is set
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bool Copter::ekf_position_ok()
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{
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if (!ahrs.have_inertial_nav()) {
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// do not allow navigation with dcm position
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return false;
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}
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// with EKF use filter status and ekf check
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nav_filter_status filt_status = inertial_nav.get_filter_status();
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// if disarmed we accept a predicted horizontal position
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if (!motors.armed()) {
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return ((filt_status.flags.horiz_pos_abs || filt_status.flags.pred_horiz_pos_abs));
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} else {
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// once armed we require a good absolute position and EKF must not be in const_pos_mode
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return (filt_status.flags.horiz_pos_abs && !filt_status.flags.const_pos_mode);
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}
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}
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// optflow_position_ok - returns true if optical flow based position estimate is ok
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bool Copter::optflow_position_ok()
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{
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#if OPTFLOW != ENABLED
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return false;
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#else
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// return immediately if optflow is not enabled or EKF not used
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if (!optflow.enabled() || !ahrs.have_inertial_nav()) {
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return false;
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}
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// get filter status from EKF
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nav_filter_status filt_status = inertial_nav.get_filter_status();
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// if disarmed we accept a predicted horizontal relative position
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if (!motors.armed()) {
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return (filt_status.flags.pred_horiz_pos_rel);
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} else {
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return (filt_status.flags.horiz_pos_rel && !filt_status.flags.const_pos_mode);
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}
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#endif
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}
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// update_auto_armed - update status of auto_armed flag
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void Copter::update_auto_armed()
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{
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// disarm checks
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if(ap.auto_armed){
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// if motors are disarmed, auto_armed should also be false
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if(!motors.armed()) {
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set_auto_armed(false);
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return;
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}
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// if in stabilize or acro flight mode and throttle is zero, auto-armed should become false
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if(mode_has_manual_throttle(control_mode) && ap.throttle_zero && !failsafe.radio) {
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set_auto_armed(false);
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}
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#if FRAME_CONFIG == HELI_FRAME
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// if helicopters are on the ground, and the motor is switched off, auto-armed should be false
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// so that rotor runup is checked again before attempting to take-off
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if(ap.land_complete && !motors.rotor_runup_complete()) {
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set_auto_armed(false);
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}
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#endif // HELI_FRAME
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}else{
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// arm checks
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#if FRAME_CONFIG == HELI_FRAME
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// for tradheli if motors are armed and throttle is above zero and the motor is started, auto_armed should be true
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if(motors.armed() && !ap.throttle_zero && motors.rotor_runup_complete()) {
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set_auto_armed(true);
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}
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#else
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// if motors are armed and throttle is above zero auto_armed should be true
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if(motors.armed() && !ap.throttle_zero) {
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set_auto_armed(true);
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}
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#endif // HELI_FRAME
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}
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}
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void Copter::check_usb_mux(void)
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{
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bool usb_check = hal.gpio->usb_connected();
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if (usb_check == ap.usb_connected) {
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return;
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}
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// the user has switched to/from the telemetry port
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ap.usb_connected = usb_check;
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}
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// frsky_telemetry_send - sends telemetry data using frsky telemetry
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// should be called at 5Hz by scheduler
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#if FRSKY_TELEM_ENABLED == ENABLED
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void Copter::frsky_telemetry_send(void)
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{
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frsky_telemetry.send_frames((uint8_t)control_mode);
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}
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#endif
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/*
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should we log a message type now?
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*/
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bool Copter::should_log(uint32_t mask)
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{
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#if LOGGING_ENABLED == ENABLED
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if (!(mask & g.log_bitmask) || in_mavlink_delay) {
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return false;
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}
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bool ret = motors.armed() || (g.log_bitmask & MASK_LOG_WHEN_DISARMED) != 0;
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if (ret && !DataFlash.logging_started() && !in_log_download) {
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start_logging();
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}
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return ret;
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#else
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return false;
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#endif
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}
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