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 |
WO2008108787(A3) |
申请公布日期 |
2008.11.13 |
申请号 |
WO2007US12890 |
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 |
G05D1/00 |
主分类号 |
G05D1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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