发明名称 |
SURFACE CONTACT OVERRIDE LANDING SCHEME FOR A FBW ROTARY-WING AIRCRAFT |
摘要 |
A method of transitioning from a complex response flight state to a ground operation control state. Pilot intent is determined through collective position information to control the transition. An independent cockpit switch activates an emergency surface contact transition function for use with a fly-by-wire (FBW) flight control system. Once the surface contact transition function is active, FBW control laws transition from a fully augmented flight state, through an augmentation deactivation state and into the surface contact state. |
申请公布号 |
EP2033059(A2) |
申请公布日期 |
2009.03.11 |
申请号 |
EP20070873878 |
申请日期 |
2007.05.31 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
FANCIULLO, TODD;MORPHY, PAUL;STILES, LORREN;FAYNBERG, ALEX |
分类号 |
G05D1/06;B64C13/50;G01C23/00;G05D1/08 |
主分类号 |
G05D1/06 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|