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https://github.com/ArduPilot/ardupilot
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AP_HAL_SITL: move SITL Compass to standard sensor backend model
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@ -88,7 +88,6 @@ void SITL_State::_sitl_setup(const char *home_str)
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// setup some initial values
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#ifndef HIL_MODE
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_update_airspeed(0);
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_update_compass();
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_update_gps(0, 0, 0, 0, 0, 0, false);
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_update_rangefinder(0);
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#endif
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@ -167,7 +166,6 @@ void SITL_State::_fdm_input_step(void)
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_sitl->state.speedN, _sitl->state.speedE, _sitl->state.speedD,
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!_sitl->gps_disable);
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_update_airspeed(_sitl->state.airspeed);
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_update_compass();
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_update_rangefinder(_sitl->state.range);
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if (_sitl->adsb_plane_count >= 0 &&
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@ -431,20 +429,6 @@ void SITL_State::_simulator_servos(SITL::Aircraft::sitl_input &input)
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current_pin_value = ((_current / 17.0f) / 5.0f) * 1024;
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}
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// generate a random Vector3f of size 1
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Vector3f SITL_State::_rand_vec3f(void)
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{
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Vector3f v = Vector3f(rand_float(),
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rand_float(),
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rand_float());
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if (v.length() != 0.0f) {
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v.normalize();
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}
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return v;
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}
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void SITL_State::init(int argc, char * const argv[])
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{
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pwm_input[0] = pwm_input[1] = pwm_input[3] = 1500;
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@ -83,7 +83,6 @@ private:
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void _setup_adc(void);
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void set_height_agl(void);
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void _update_compass(void);
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void _update_rangefinder(float range_value);
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void _set_signal_handlers(void) const;
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@ -131,7 +130,6 @@ private:
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void _simulator_output(bool synthetic_clock_mode);
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uint16_t _airspeed_sensor(float airspeed);
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uint16_t _ground_sonar();
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Vector3f _rand_vec3f(void);
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void _fdm_input_step(void);
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void wait_clock(uint64_t wait_time_usec);
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@ -1,87 +0,0 @@
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/*
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SITL handling
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This simulates a compass
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Andrew Tridgell November 2011
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*/
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#include <AP_HAL/AP_HAL.h>
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
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#include "AP_HAL_SITL.h"
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#include "AP_HAL_SITL_Namespace.h"
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#include "HAL_SITL_Class.h"
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#include <AP_Math/AP_Math.h>
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#include <AP_Compass/AP_Compass.h>
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#include <AP_Declination/AP_Declination.h>
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#include <SITL/SITL.h>
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extern const AP_HAL::HAL& hal;
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using namespace HALSITL;
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/*
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setup the compass with new input
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all inputs are in degrees
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*/
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void SITL_State::_update_compass(void)
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{
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static uint32_t last_update;
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if (_compass == nullptr) {
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// no compass in this sketch
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return;
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}
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// 100Hz
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uint32_t now = AP_HAL::millis();
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if ((now - last_update) < 10) {
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return;
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}
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last_update = now;
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// calculate sensor noise and add to 'truth' field in body frame
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// units are milli-Gauss
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Vector3f noise = _rand_vec3f() * _sitl->mag_noise;
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Vector3f new_mag_data = _sitl->state.bodyMagField + noise;
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// add delay
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uint32_t best_time_delta_mag = 1000; // initialise large time representing buffer entry closest to current time - delay.
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uint8_t best_index_mag = 0; // initialise number representing the index of the entry in buffer closest to delay.
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// storing data from sensor to buffer
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if (now - last_store_time_mag >= 10) { // store data every 10 ms.
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last_store_time_mag = now;
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if (store_index_mag > mag_buffer_length-1) { // reset buffer index if index greater than size of buffer
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store_index_mag = 0;
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}
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buffer_mag[store_index_mag].data = new_mag_data; // add data to current index
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buffer_mag[store_index_mag].time = last_store_time_mag; // add time to current index
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store_index_mag = store_index_mag + 1; // increment index
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}
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// return delayed measurement
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delayed_time_mag = now - _sitl->mag_delay; // get time corresponding to delay
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// find data corresponding to delayed time in buffer
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for (uint8_t i=0; i<=mag_buffer_length-1; i++) {
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// find difference between delayed time and time stamp in buffer
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time_delta_mag = abs((int32_t)(delayed_time_mag - buffer_mag[i].time));
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// if this difference is smaller than last delta, store this time
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if (time_delta_mag < best_time_delta_mag) {
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best_index_mag = i;
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best_time_delta_mag = time_delta_mag;
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}
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}
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if (best_time_delta_mag < 1000) { // only output stored state if < 1 sec retrieval error
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new_mag_data = buffer_mag[best_index_mag].data;
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}
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new_mag_data -= _sitl->mag_ofs.get();
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_compass->setHIL(0, new_mag_data, AP_HAL::micros());
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_compass->setHIL(1, new_mag_data, AP_HAL::micros());
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}
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#endif
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