mirror of https://github.com/ArduPilot/ardupilot
AP_InertialSensor: converted HIL backend, which gets SITL working
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448efc70a3
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@ -300,7 +300,13 @@ AP_InertialSensor::init( Start_style style,
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void
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AP_InertialSensor::_detect_backends(Sample_rate sample_rate)
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{
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#if HAL_INS_DEFAULT == HAL_INS_HIL
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_backends[0] = AP_InertialSensor_HIL::detect(*this, sample_rate, _gyro[_gyro_count], _accel[_accel_count]);
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#elif HAL_INS_DEFAULT == HAL_INS_MPU6000
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_backends[0] = AP_InertialSensor_MPU6000::detect(*this, sample_rate, _gyro[_gyro_count], _accel[_accel_count]);
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#else
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#error Unrecognised HAL_INS_TYPE setting
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#endif
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if (_backends[0] == NULL ||
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_gyro_count == 0 ||
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_accel_count == 0) {
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@ -917,9 +923,27 @@ void AP_InertialSensor::wait_for_sample(void)
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for (uint8_t i=0; i<INS_MAX_INSTANCES; i++) {
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if (_backends[i] != NULL) {
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gyro_available |= _backends[i]->gyro_sample_available();
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accel_available |= _backends[i]->gyro_sample_available();
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accel_available |= _backends[i]->accel_sample_available();
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}
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}
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hal.scheduler->delay_microseconds(100);
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hal.scheduler->delay(1);
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}
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}
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/*
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support for setting accel and gyro vectors, for use by HIL
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*/
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void AP_InertialSensor::set_accel(uint8_t instance, const Vector3f &accel)
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{
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if (instance < INS_MAX_INSTANCES) {
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_accel[instance] = accel;
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}
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}
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void AP_InertialSensor::set_gyro(uint8_t instance, const Vector3f &gyro)
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{
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if (instance < INS_MAX_INSTANCES) {
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_gyro[instance] = gyro;
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}
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}
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@ -251,6 +251,7 @@ private:
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#include "AP_InertialSensor_Backend.h"
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#include "AP_InertialSensor_MPU6000.h"
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#include "AP_InertialSensor_HIL.h"
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#include "AP_InertialSensor_UserInteract_Stream.h"
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#include "AP_InertialSensor_UserInteract_MAVLink.h"
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@ -1,132 +1,71 @@
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#if NOT_YET
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#include "AP_InertialSensor_HIL.h"
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#include <AP_HAL.h>
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#include "AP_InertialSensor_HIL.h"
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const extern AP_HAL::HAL& hal;
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AP_InertialSensor_HIL::AP_InertialSensor_HIL() :
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AP_InertialSensor(),
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AP_InertialSensor_HIL::AP_InertialSensor_HIL(AP_InertialSensor &imu, Vector3f &gyro, Vector3f &accel) :
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AP_InertialSensor_Backend(imu, gyro, accel),
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_sample_period_usec(0),
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_last_sample_usec(0)
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{
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_accel[0] = Vector3f(0, 0, -GRAVITY_MSS);
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}
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uint16_t AP_InertialSensor_HIL::_init_sensor( Sample_rate sample_rate ) {
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/*
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detect the sensor
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*/
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AP_InertialSensor_Backend *AP_InertialSensor_HIL::detect(AP_InertialSensor &_imu,
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AP_InertialSensor::Sample_rate sample_rate,
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Vector3f &gyro,
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Vector3f &accel)
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{
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AP_InertialSensor_HIL *sensor = new AP_InertialSensor_HIL(_imu, gyro, accel);
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if (sensor == NULL) {
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return NULL;
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}
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if (!sensor->_init_sensor(sample_rate)) {
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delete sensor;
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return NULL;
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}
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return sensor;
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}
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bool AP_InertialSensor_HIL::_init_sensor(AP_InertialSensor::Sample_rate sample_rate)
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{
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switch (sample_rate) {
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case RATE_50HZ:
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case AP_InertialSensor::RATE_50HZ:
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_sample_period_usec = 20000;
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break;
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case RATE_100HZ:
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case AP_InertialSensor::RATE_100HZ:
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_sample_period_usec = 10000;
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break;
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case RATE_200HZ:
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case AP_InertialSensor::RATE_200HZ:
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_sample_period_usec = 5000;
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break;
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case RATE_400HZ:
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case AP_InertialSensor::RATE_400HZ:
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_sample_period_usec = 2500;
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break;
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}
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return AP_PRODUCT_ID_NONE;
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}
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/*================ AP_INERTIALSENSOR PUBLIC INTERFACE ==================== */
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// grab the used instances
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_imu.register_gyro();
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_imu.register_accel();
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bool AP_InertialSensor_HIL::update( void ) {
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uint32_t now = hal.scheduler->micros();
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_last_sample_usec = now;
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return true;
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}
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float AP_InertialSensor_HIL::get_delta_time() const {
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return _sample_period_usec * 1.0e-6f;
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}
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float AP_InertialSensor_HIL::get_gyro_drift_rate(void) {
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// 0.5 degrees/second/minute
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return ToRad(0.5/60);
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bool AP_InertialSensor_HIL::update(void)
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{
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uint32_t now = hal.scheduler->micros();
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while (now - _last_sample_usec > _sample_period_usec) {
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_last_sample_usec += _sample_period_usec;
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}
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return true;
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}
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bool AP_InertialSensor_HIL::_sample_available()
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{
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uint32_t tnow = hal.scheduler->micros();
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bool have_sample = false;
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while (tnow - _last_sample_usec > _sample_period_usec) {
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have_sample = true;
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_last_sample_usec += _sample_period_usec;
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}
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return have_sample;
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return (hal.scheduler->micros() - _last_sample_usec > _sample_period_usec);
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}
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bool AP_InertialSensor_HIL::wait_for_sample(uint16_t timeout_ms)
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{
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if (_sample_available()) {
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return true;
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}
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uint32_t start = hal.scheduler->millis();
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while ((hal.scheduler->millis() - start) < timeout_ms) {
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uint32_t tnow = hal.scheduler->micros();
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uint32_t tdelay = (_last_sample_usec + _sample_period_usec) - tnow;
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if (tdelay < 100000) {
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hal.scheduler->delay_microseconds(tdelay);
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}
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if (_sample_available()) {
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return true;
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}
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}
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return false;
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}
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void AP_InertialSensor_HIL::set_accel(uint8_t instance, const Vector3f &accel)
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{
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if (instance >= INS_MAX_INSTANCES) {
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return;
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}
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_previous_accel[instance] = _accel[instance];
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_accel[instance] = accel;
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_last_accel_usec[instance] = hal.scheduler->micros();
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}
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void AP_InertialSensor_HIL::set_gyro(uint8_t instance, const Vector3f &gyro)
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{
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if (instance >= INS_MAX_INSTANCES) {
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return;
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}
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_gyro[instance] = gyro;
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_last_gyro_usec[instance] = hal.scheduler->micros();
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}
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bool AP_InertialSensor_HIL::get_gyro_health(uint8_t instance) const
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{
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if (instance >= INS_MAX_INSTANCES) {
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return false;
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}
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return (hal.scheduler->micros() - _last_gyro_usec[instance]) < 40000;
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}
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bool AP_InertialSensor_HIL::get_accel_health(uint8_t instance) const
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{
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if (instance >= INS_MAX_INSTANCES) {
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return false;
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}
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return (hal.scheduler->micros() - _last_accel_usec[instance]) < 40000;
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}
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uint8_t AP_InertialSensor_HIL::get_gyro_count(void) const
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{
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if (get_gyro_health(1)) {
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return 2;
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}
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return 1;
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}
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uint8_t AP_InertialSensor_HIL::get_accel_count(void) const
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{
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if (get_accel_health(1)) {
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return 2;
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}
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return 1;
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}
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#endif
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@ -1,36 +1,32 @@
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#ifndef __AP_INERTIAL_SENSOR_STUB_H__
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#define __AP_INERTIAL_SENSOR_STUB_H__
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#ifndef __AP_INERTIALSENSOR_HIL_H__
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#define __AP_INERTIALSENSOR_HIL_H__
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#include <AP_Progmem.h>
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#include "AP_InertialSensor.h"
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class AP_InertialSensor_HIL : public AP_InertialSensor
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class AP_InertialSensor_HIL : public AP_InertialSensor_Backend
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{
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public:
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AP_InertialSensor_HIL(AP_InertialSensor &imu, Vector3f &gyro, Vector3f &accel);
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AP_InertialSensor_HIL();
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/* update accel and gyro state */
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bool update();
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/* Concrete implementation of AP_InertialSensor functions: */
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bool update();
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float get_delta_time() const;
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float get_gyro_drift_rate();
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bool wait_for_sample(uint16_t timeout_ms);
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void set_accel(uint8_t instance, const Vector3f &accel);
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void set_gyro(uint8_t instance, const Vector3f &gyro);
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bool get_gyro_health(uint8_t instance) const;
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bool get_accel_health(uint8_t instance) const;
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uint8_t get_gyro_count(void) const;
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uint8_t get_accel_count(void) const;
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bool gyro_sample_available(void) { return _sample_available(); }
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bool accel_sample_available(void) { return _sample_available(); }
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// detect the sensor
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static AP_InertialSensor_Backend *detect(AP_InertialSensor &imu,
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AP_InertialSensor::Sample_rate sample_rate,
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Vector3f &gyro,
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Vector3f &accel);
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private:
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bool _sample_available();
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uint16_t _init_sensor( Sample_rate sample_rate );
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uint32_t _sample_period_usec;
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uint32_t _last_sample_usec;
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uint32_t _last_accel_usec[INS_MAX_INSTANCES];
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uint32_t _last_gyro_usec[INS_MAX_INSTANCES];
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bool _init_sensor(AP_InertialSensor::Sample_rate sample_rate);
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bool _sample_available(void);
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uint32_t _sample_period_usec;
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uint32_t _last_sample_usec;
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};
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#endif // __AP_INERTIAL_SENSOR_STUB_H__
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#endif // __AP_INERTIALSENSOR_HIL_H__
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