mirror of https://github.com/ArduPilot/ardupilot
340 lines
10 KiB
C++
340 lines
10 KiB
C++
#include "Blimp.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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static void failsafe_check_static()
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{
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blimp.failsafe_check();
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}
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void Blimp::init_ardupilot()
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{
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#if STATS_ENABLED == ENABLED
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// initialise stats module
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g2.stats.init();
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#endif
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BoardConfig.init();
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// initialise notify system
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notify.init();
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notify_flight_mode();
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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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// setup telem slots with serial ports
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gcs().setup_uarts();
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#if LOGGING_ENABLED == ENABLED
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log_init();
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#endif
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init_rc_in(); // sets up rc channels from radio
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// allocate the motors class
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allocate_motors();
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// initialise rc channels including setting mode
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rc().init();
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// sets up motors and output to escs
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init_rc_out();
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// motors initialised so parameters can be sent
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ap.initialised_params = true;
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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.set_log_gps_bit(MASK_LOG_GPS);
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gps.init(serial_manager);
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AP::compass().set_log_bit(MASK_LOG_COMPASS);
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AP::compass().init();
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// attitude_control->parameter_sanity_check();
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// pos_control->set_dt(scheduler.get_loop_period_s());
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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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barometer.set_log_baro_bit(MASK_LOG_IMU);
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barometer.calibrate();
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// #if MODE_AUTO_ENABLED == ENABLED
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// // initialise mission library
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// mode_auto.mission.init();
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// #endif
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// initialise AP_Logger library
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logger.setVehicle_Startup_Writer(FUNCTOR_BIND(&blimp, &Blimp::Log_Write_Vehicle_Startup_Messages, void));
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startup_INS_ground();
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#ifdef ENABLE_SCRIPTING
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g2.scripting.init();
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#endif // ENABLE_SCRIPTING
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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_log_raw_bit(MASK_LOG_IMU_RAW);
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// setup fin output
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motors->setup_fins();
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// enable output to motors
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if (arming.rc_calibration_checks(true)) {
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enable_motor_output();
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}
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// attempt to switch to MANUAL, if this fails then switch to Land
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if (!set_mode((enum Mode::Number)g.initial_mode.get(), ModeReason::INITIALISED)) {
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// set mode to MANUAL will trigger mode change notification to pilot
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set_mode(Mode::Number::MANUAL, ModeReason::UNAVAILABLE);
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} else {
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// alert pilot to mode change
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AP_Notify::events.failsafe_mode_change = 1;
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}
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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 Blimp::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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// position_ok - returns true if the horizontal absolute position is ok and home position is set
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bool Blimp::position_ok() const
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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_has_absolute_position() || ekf_has_relative_position());
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}
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// ekf_has_absolute_position - returns true if the EKF can provide an absolute WGS-84 position estimate
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bool Blimp::ekf_has_absolute_position() const
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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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// ekf_has_relative_position - returns true if the EKF can provide a position estimate relative to it's starting position
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bool Blimp::ekf_has_relative_position() const
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{
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// return immediately if EKF not used
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if (!ahrs.have_inertial_nav()) {
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return false;
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}
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// return immediately if neither optflow nor visual odometry is enabled
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bool enabled = false;
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// #if OPTFLOW == ENABLED
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// if (optflow.enabled()) {
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// enabled = true;
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// }
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// #endif
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// #if HAL_VISUALODOM_ENABLED
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// if (visual_odom.enabled()) {
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// enabled = true;
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// }
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// #endif
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if (!enabled) {
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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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}
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// returns true if the ekf has a good altitude estimate (required for modes which do AltHold)
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bool Blimp::ekf_alt_ok() const
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{
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if (!ahrs.have_inertial_nav()) {
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// do not allow alt control with only dcm
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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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// require both vertical velocity and position
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return (filt_status.flags.vert_vel && filt_status.flags.vert_pos);
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}
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// update_auto_armed - update status of auto_armed flag
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void Blimp::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 (flightmode->has_manual_throttle() && ap.throttle_zero && !failsafe.radio) {
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set_auto_armed(false);
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}
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// if heliblimps 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->get_spool_state() != Fins::SpoolState::THROTTLE_UNLIMITED && ap.using_interlock) {
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set_auto_armed(false);
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}
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}
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}
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/*
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should we log a message type now?
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*/
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bool Blimp::should_log(uint32_t mask)
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{
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#if LOGGING_ENABLED == ENABLED
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ap.logging_started = logger.logging_started();
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return logger.should_log(mask);
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#else
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return false;
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#endif
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}
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// return MAV_TYPE corresponding to frame class
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MAV_TYPE Blimp::get_frame_mav_type()
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{
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return MAV_TYPE_QUADROTOR; //TODO: Mavlink changes to allow type to be correct
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}
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// return string corresponding to frame_class
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const char* Blimp::get_frame_string()
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{
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return "AIRFISH"; //TODO: Change to be able to change with different frame_classes
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}
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/*
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allocate the motors class
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*/
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void Blimp::allocate_motors(void)
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{
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switch ((Fins::motor_frame_class)g2.frame_class.get()) {
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case Fins::MOTOR_FRAME_AIRFISH:
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default:
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motors = new Fins(blimp.scheduler.get_loop_rate_hz());
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break;
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}
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if (motors == nullptr) {
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AP_HAL::panic("Unable to allocate FRAME_CLASS=%u", (unsigned)g2.frame_class.get());
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}
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AP_Param::load_object_from_eeprom(motors, Fins::var_info);
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// const struct AP_Param::GroupInfo *ac_var_info;
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// attitude_control = new AC_AttitudeControl_Multi(*ahrs_view, aparm, *motors, scheduler.get_loop_period_s());
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// ac_var_info = AC_AttitudeControl_Multi::var_info;
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// if (attitude_control == nullptr) {
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// AP_HAL::panic("Unable to allocate AttitudeControl");
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// }
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// AP_Param::load_object_from_eeprom(attitude_control, ac_var_info);
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// pos_control = new AC_PosControl(*ahrs_view, inertial_nav, *motors, *attitude_control);
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// if (pos_control == nullptr) {
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// AP_HAL::panic("Unable to allocate PosControl");
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// }
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// AP_Param::load_object_from_eeprom(pos_control, pos_control->var_info);
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// wp_nav = new AC_WPNav(inertial_nav, *ahrs_view, *pos_control, *attitude_control);
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// if (wp_nav == nullptr) {
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// AP_HAL::panic("Unable to allocate WPNav");
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// }
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// AP_Param::load_object_from_eeprom(wp_nav, wp_nav->var_info);
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// loiter_nav = new AC_Loiter(inertial_nav, *ahrs_view, *pos_control, *attitude_control);
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// if (loiter_nav == nullptr) {
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// AP_HAL::panic("Unable to allocate LoiterNav");
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// }
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// AP_Param::load_object_from_eeprom(loiter_nav, loiter_nav->var_info);
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// reload lines from the defaults file that may now be accessible
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AP_Param::reload_defaults_file(true);
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// param count could have changed
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AP_Param::invalidate_count();
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}
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