| 发明名称 | Systems for inceptor control in fly-by-wire aircraft systems | ||
| 摘要 | Aircraft, control-by-wire systems, and controllers are provided. The aircraft includes a flight control surface and a control-by-wire system. The control-by-wire system includes an input device and a controller. The input device is configured to control the flight control surface. The controller is communicatively coupled with the input device and configured to automatically offset a neutral force position of the input device based on a deviation of the aircraft from a reference condition while the aircraft is operated in a manual flight mode. | ||
| 申请公布号 | US9446838(B2) | 申请公布日期 | 2016.09.20 |
| 申请号 | US201414459566 | 申请日期 | 2014.08.14 |
| 申请人 | Gulfstream Aerospace Corporation | 发明人 | Buethe Scott;Hartley Robert;Hugon Francois;Landers Thomas |
| 分类号 | B64C13/50;G05D1/00 | 主分类号 | B64C13/50 |
| 代理机构 | Lorenz & Kopf, LLP (LKGlobal) | 代理人 | Lorenz & Kopf, LLP (LKGlobal) |
| 主权项 | 1. An aircraft comprising: a flight control surface; and a control-by-wire system comprising: an input device configured to control the flight control surface; and a controller communicatively coupled with the input device and configured to automatically offset a neutral force position of the input device based on a deviation of the aircraft from a reference condition while the aircraft is operated in a manual flight mode. | ||
| 地址 | Savannah GA US | ||