System and method for optimizing horizontal tail loads |
|||||||
| 申请号 | US14278868 | 申请日 | 2014-05-15 | 公开(公告)号 | US09878776B2 | 公开(公告)日 | 2018-01-30 |
| 申请人 | The Boeing Company; | 发明人 | Vedad Mahmulyin; | ||||
| 摘要 | A method of controlling an elevator of an aircraft may include identifying a current stabilizer angle of incidence of a stabilizer of the aircraft. The stabilizer may include an elevator pivotably coupled to the stabilizer. The method may further include comparing the current stabilizer angle of incidence with a threshold stabilizer angle of incidence, and selecting an elevator position limit that is more restrictive if the current stabilizer angle of incidence is greater than or equal to the threshold stabilizer angle of incidence. The method may additionally include moving the elevator to a commanded elevator position that is no greater than the elevator position limit. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
QQ群二维码
意见反馈
意见反馈