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AP_AHRS: fix attitudes_consistent bug
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@ -1325,7 +1325,7 @@ bool AP_AHRS_NavEKF::attitudes_consistent(char *failure_msg, const uint8_t failu
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for (uint8_t i = 0; i < EKF2.activeCores(); i++) {
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for (uint8_t i = 0; i < EKF2.activeCores(); i++) {
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Quaternion ekf2_quat;
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Quaternion ekf2_quat;
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Vector3f angle_diff;
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Vector3f angle_diff;
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EKF2.getQuaternion(i, ekf2_quat);
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EKF2.getQuaternionBodyToNED(i, ekf2_quat);
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primary_quat.angular_difference(ekf2_quat).to_axis_angle(angle_diff);
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primary_quat.angular_difference(ekf2_quat).to_axis_angle(angle_diff);
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float diff = safe_sqrt(sq(angle_diff.x)+sq(angle_diff.y));
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float diff = safe_sqrt(sq(angle_diff.x)+sq(angle_diff.y));
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if (diff > ATTITUDE_CHECK_THRESH_ROLL_PITCH_RAD) {
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if (diff > ATTITUDE_CHECK_THRESH_ROLL_PITCH_RAD) {
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@ -1343,7 +1343,7 @@ bool AP_AHRS_NavEKF::attitudes_consistent(char *failure_msg, const uint8_t failu
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for (uint8_t i = 0; i < EKF3.activeCores(); i++) {
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for (uint8_t i = 0; i < EKF3.activeCores(); i++) {
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Quaternion ekf3_quat;
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Quaternion ekf3_quat;
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Vector3f angle_diff;
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Vector3f angle_diff;
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EKF3.getQuaternion(i, ekf3_quat);
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EKF3.getQuaternionBodyToNED(i, ekf3_quat);
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primary_quat.angular_difference(ekf3_quat).to_axis_angle(angle_diff);
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primary_quat.angular_difference(ekf3_quat).to_axis_angle(angle_diff);
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float diff = safe_sqrt(sq(angle_diff.x)+sq(angle_diff.y));
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float diff = safe_sqrt(sq(angle_diff.x)+sq(angle_diff.y));
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if (diff > ATTITUDE_CHECK_THRESH_ROLL_PITCH_RAD) {
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if (diff > ATTITUDE_CHECK_THRESH_ROLL_PITCH_RAD) {
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