PILOT ACTIVATED TRIM FOR FLY-BY-WIRE AIRCRAFT |
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| 申请号 | US15404804 | 申请日 | 2017-01-12 | 公开(公告)号 | US20170197705A1 | 公开(公告)日 | 2017-07-13 |
| 申请人 | Sikorsky Aircraft Corporation; | 发明人 | Leonard M. Wengler, III; Kevin L. Bredenbeck; Matthew T. Luszcz; Matthew A. White; William Fell; | ||||
| 摘要 | A fly-by-wire aircraft and method of flying a fly-by-wire aircraft is disclosed. The aircraft includes a control system for flying the aircraft in one of a proportional ground control mode and a model following controls mode. A control device at a control interface of the aircraft selectively activates a trim follow up function in the control system. When flying the aircraft in a proportional ground control mode, trim follow up function can be activated. The control system can then transition into the model following controls mode with the trim follow up function activated to reduce transient behavior. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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