Stability and control augmentation system

申请号 US14632044 申请日 2015-02-26 公开(公告)号 US10037040B2 公开(公告)日 2018-07-31
申请人 Goodrich Actuation Systems SAS; 发明人 Arnauld R. E. Hervieux; Gregory Y. Meignat;
摘要 A Stability and Command Augmentation System (SCAS) for an aircraft, the SCAS including, a first input shaft providing a first rotational input; a second input shaft providing a second rotational input; and a device for summing the first and second rotational inputs to give a rotational output for controlling an actuator. A method of operating a SCAS on an aircraft, the method including providing a pilot input order in the form of a rotating first shaft, providing an augmentation input order in the form of a rotating second shaft, summing the rotation of the pilot input order and the augmentation input order to give an output order; and using the output order to control an actuator.
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