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@ -116,6 +116,21 @@ AP_AHRS_DCM::update(bool skip_ins_update)
@@ -116,6 +116,21 @@ AP_AHRS_DCM::update(bool skip_ins_update)
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// update AOA and SSA
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update_AOA_SSA(); |
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backup_attitude(); |
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} |
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/*
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backup attitude to stm32 registers at 3Hz |
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*/ |
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void AP_AHRS_DCM::backup_attitude(void) |
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{ |
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uint32_t now = AP_HAL::millis(); |
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if (now - _last_backup_ms < 333) { |
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return; |
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} |
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_last_backup_ms = now; |
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hal.util->set_backup_attitude(roll_sensor, pitch_sensor, yaw_sensor); |
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} |
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// update the DCM matrix using only the gyros
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@ -175,7 +190,16 @@ AP_AHRS_DCM::reset(bool recover_eulers)
@@ -175,7 +190,16 @@ AP_AHRS_DCM::reset(bool recover_eulers)
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// if the caller wants us to try to recover to the current
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// attitude then calculate the dcm matrix from the current
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// roll/pitch/yaw values
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if (recover_eulers && !isnan(roll) && !isnan(pitch) && !isnan(yaw)) { |
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if (hal.util->was_watchdog_reset() && |
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hal.util->get_backup_attitude(roll_sensor, pitch_sensor, yaw_sensor) && |
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AP_HAL::millis() < 10000) { |
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roll = radians(roll_sensor*0.01f); |
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pitch = radians(pitch_sensor*0.01f); |
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yaw = radians(yaw_sensor*0.01f); |
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_dcm_matrix.from_euler(roll, pitch, yaw); |
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gcs().send_text(MAV_SEVERITY_INFO, "Restored watchdog attitude %d %d %d", |
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roll_sensor/100, pitch_sensor/100, yaw_sensor/100); |
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} else if (recover_eulers && !isnan(roll) && !isnan(pitch) && !isnan(yaw)) { |
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_dcm_matrix.from_euler(roll, pitch, yaw); |
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} else { |
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