mirror of https://github.com/ArduPilot/ardupilot
AP_AHRS_DCM: use millis/micros/panic functions
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@ -53,7 +53,7 @@ AP_AHRS_DCM::update(void)
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float delta_t;
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if (_last_startup_ms == 0) {
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_last_startup_ms = hal.scheduler->millis();
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_last_startup_ms = AP_HAL::millis();
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}
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// tell the IMU to grab some data
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@ -177,7 +177,7 @@ AP_AHRS_DCM::reset(bool recover_eulers)
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}
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_last_startup_ms = hal.scheduler->millis();
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_last_startup_ms = AP_HAL::millis();
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}
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// reset the current attitude, used by HIL
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@ -292,7 +292,7 @@ AP_AHRS_DCM::normalize(void)
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!renorm(t2, _dcm_matrix.c)) {
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// Our solution is blowing up and we will force back
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// to last euler angles
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_last_failure_ms = hal.scheduler->millis();
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_last_failure_ms = AP_HAL::millis();
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AP_AHRS_DCM::reset(true);
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}
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}
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@ -382,7 +382,7 @@ bool AP_AHRS_DCM::have_gps(void) const
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*/
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bool AP_AHRS_DCM::use_fast_gains(void) const
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{
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return !hal.util->get_soft_armed() && (hal.scheduler->millis() - _last_startup_ms) < 20000U;
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return !hal.util->get_soft_armed() && (AP_HAL::millis() - _last_startup_ms) < 20000U;
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}
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@ -408,13 +408,13 @@ bool AP_AHRS_DCM::use_compass(void)
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// prevent flyaways with very bad compass offsets
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int32_t error = abs(wrap_180_cd(yaw_sensor - _gps.ground_course_cd()));
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if (error > 4500 && _wind.length() < _gps.ground_speed()*0.8f) {
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if (hal.scheduler->millis() - _last_consistent_heading > 2000) {
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if (AP_HAL::millis() - _last_consistent_heading > 2000) {
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// start using the GPS for heading if the compass has been
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// inconsistent with the GPS for 2 seconds
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return false;
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}
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} else {
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_last_consistent_heading = hal.scheduler->millis();
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_last_consistent_heading = AP_HAL::millis();
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}
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// use the compass
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@ -637,7 +637,7 @@ AP_AHRS_DCM::drift_correction(float deltat)
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// add in wind estimate
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velocity += _wind;
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last_correction_time = hal.scheduler->millis();
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last_correction_time = AP_HAL::millis();
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_have_gps_lock = false;
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} else {
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if (_gps.last_fix_time_ms() == _ra_sum_start) {
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@ -703,7 +703,7 @@ AP_AHRS_DCM::drift_correction(float deltat)
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GA_e.normalize();
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if (GA_e.is_inf()) {
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// wait for some non-zero acceleration information
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_last_failure_ms = hal.scheduler->millis();
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_last_failure_ms = AP_HAL::millis();
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return;
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}
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using_gps_corrections = true;
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@ -762,7 +762,7 @@ AP_AHRS_DCM::drift_correction(float deltat)
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if (besti == -1) {
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// no healthy accelerometers!
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_last_failure_ms = hal.scheduler->millis();
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_last_failure_ms = AP_HAL::millis();
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return;
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}
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@ -812,7 +812,7 @@ AP_AHRS_DCM::drift_correction(float deltat)
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if (error[besti].is_nan() || error[besti].is_inf()) {
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// don't allow bad values
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check_matrix();
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_last_failure_ms = hal.scheduler->millis();
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_last_failure_ms = AP_HAL::millis();
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return;
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}
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@ -887,7 +887,7 @@ void AP_AHRS_DCM::estimate_wind(void)
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// See http://gentlenav.googlecode.com/files/WindEstimation.pdf
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Vector3f fuselageDirection = _dcm_matrix.colx();
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Vector3f fuselageDirectionDiff = fuselageDirection - _last_fuse;
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uint32_t now = hal.scheduler->millis();
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uint32_t now = AP_HAL::millis();
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// scrap our data and start over if we're taking too long to get a direction change
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if (now - _last_wind_time > 10000) {
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@ -1011,7 +1011,7 @@ void AP_AHRS_DCM::set_home(const Location &loc)
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bool AP_AHRS_DCM::healthy(void) const
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{
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// consider ourselves healthy if there have been no failures for 5 seconds
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return (_last_failure_ms == 0 || hal.scheduler->millis() - _last_failure_ms > 5000);
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return (_last_failure_ms == 0 || AP_HAL::millis() - _last_failure_ms > 5000);
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}
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/*
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@ -1022,5 +1022,5 @@ uint32_t AP_AHRS_DCM::uptime_ms(void) const
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if (_last_startup_ms == 0) {
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return 0;
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}
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return hal.scheduler->millis() - _last_startup_ms;
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return AP_HAL::millis() - _last_startup_ms;
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}
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