forked from Archive/PX4-Autopilot
copy quaternion setpoint into attitude setpoint topic
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ea8ba79481
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5cf8efcc60
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@ -1285,6 +1285,11 @@ MulticopterPositionControl::task_main()
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memcpy(&_att_sp.R_body[0], R.data, sizeof(_att_sp.R_body));
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_att_sp.R_valid = true;
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/* copy quaternion setpoint to attitude setpoint topic */
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math::Quaternion q_sp;
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q_sp.from_dcm(R);
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memcpy(&_att_sp.q_d[0], &q_sp.data[0], sizeof(_att_sp.q_d));
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/* calculate euler angles, for logging only, must not be used for control */
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math::Vector<3> euler = R.to_euler();
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_att_sp.roll_body = euler(0);
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@ -1300,6 +1305,11 @@ MulticopterPositionControl::task_main()
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memcpy(&_att_sp.R_body[0], R.data, sizeof(_att_sp.R_body));
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_att_sp.R_valid = true;
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/* copy quaternion setpoint to attitude setpoint topic */
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math::Quaternion q_sp;
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q_sp.from_dcm(R);
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memcpy(&_att_sp.q_d[0], &q_sp.data[0], sizeof(_att_sp.q_d));
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_att_sp.roll_body = 0.0f;
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_att_sp.pitch_body = 0.0f;
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}
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@ -1385,6 +1395,11 @@ MulticopterPositionControl::task_main()
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math::Matrix<3,3> R_sp;
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R_sp.from_euler(_att_sp.roll_body,_att_sp.pitch_body,_att_sp.yaw_body);
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memcpy(&_att_sp.R_body[0], R_sp.data, sizeof(_att_sp.R_body));
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/* copy quaternion setpoint to attitude setpoint topic */
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math::Quaternion q_sp;
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q_sp.from_dcm(R_sp);
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memcpy(&_att_sp.q_d[0], &q_sp.data[0], sizeof(_att_sp.q_d));
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_att_sp.timestamp = hrt_absolute_time();
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}
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else {
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