公开(公告)号：US20170361941A1

公开(公告)日：2017-12-21

申请号：US15184196

申请日：2016-06-16

申请人： GE Aviation Systems LLC

发明人： Steven Louis Kiebles ,  David Michael Lax ,  Otto Y. Darias ,  Mark Lawrence Darnell ,  Sean Sanghyun Hwang ,  Christopher Daniel Holbert ,  Harry Kirk Mathews, JR. ,  Sridhar Adibhatla ,  Jeffrey Russell Bult ,  Thomas Charles Swager

IPC分类号： B64D31/06 ,  B64C15/02 ,  B64D45/00 ,  G05D1/08

CPC分类号： B64D31/06 ,  B64C15/02 ,  B64D45/00 ,  G05D1/0808 ,  G05D1/0816

摘要： Systems and methods for stabilizing an aircraft in response to a yaw movement are provided. In one embodiment, a method includes detecting a yaw movement of the aircraft. The yaw movement can cause a front portion of the aircraft to move towards a first side of the aircraft. The method can further include, in response to the yaw movement, initiating a trim process resulting in a thrust differential. The trim process can include increasing thrust in one or more engines on the first side of the aircraft and decreasing thrust in one or more engines on a second side of the aircraft. The method can include controlling the trim process based at least in part on a detected yaw movement of the aircraft.