mirror of https://github.com/ArduPilot/ardupilot
57 lines
1.5 KiB
C++
57 lines
1.5 KiB
C++
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#include "Sub.h"
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#define LAND_END_DEPTH -20 //Landed at 20cm depth
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// counter to verify landings
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static uint32_t land_detector_count = 0;
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// run land and crash detectors
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// called at MAIN_LOOP_RATE
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void Sub::update_land_and_crash_detectors()
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{
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// update 1hz filtered acceleration
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Vector3f accel_ef = ahrs.get_accel_ef_blended();
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accel_ef.z += GRAVITY_MSS;
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land_accel_ef_filter.apply(accel_ef, MAIN_LOOP_SECONDS);
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update_land_detector();
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crash_check();
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}
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// update_land_detector - checks if we have landed and updates the ap.land_complete flag
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// called at MAIN_LOOP_RATE
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void Sub::update_land_detector()
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{
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if(barometer.num_instances() > 1 && barometer.get_altitude() > LAND_END_DEPTH && ap.throttle_zero) {
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set_land_complete(true);
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} else {
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set_land_complete(false);
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}
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}
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void Sub::set_land_complete(bool b)
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{
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// if no change, exit immediately
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if( ap.land_complete == b )
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return;
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land_detector_count = 0;
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if(b){
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Log_Write_Event(DATA_LAND_COMPLETE);
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} else {
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Log_Write_Event(DATA_NOT_LANDED);
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}
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ap.land_complete = b;
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}
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// update_throttle_thr_mix - sets motors throttle_low_comp value depending upon vehicle state
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// low values favour pilot/autopilot throttle over attitude control, high values favour attitude control over throttle
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// has no effect when throttle is above hover throttle
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void Sub::update_throttle_thr_mix()
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{
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return; // placeholder, was used by heli only
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}
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