发明名称 Automatic guidance system for flight vehicle having parafoil and navigation guidance apparatus for the system
摘要 An automatic guidance system guides a flight vehicle having a para foil to a target grounding point. The system opens the para foil of the flight vehicle dropped in a predetermined area above the target grounding point. The system estimates wind velocity and wind direction after the para foil of the flight vehicle is opened. Then, the system determines the landing flight path of the flight vehicle based on the estimated wind velocity and wind direction, guides the flight of the flight vehicle to the determined landing flight path and descends the flight vehicle according to the landing flight path.
申请公布号 US6343244(B1) 申请公布日期 2002.01.29
申请号 US19990444834 申请日期 1999.11.22
申请人 FUJI JUKOGYO KABUSHIKI KAISHA 发明人 YONEDA HIROSHI;AMITO ATSUSHI
分类号 B64C13/18;B64C31/02;B64C39/02;B64D17/10;G05D1/10;(IPC1-7):G06F17/00 主分类号 B64C13/18
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