发明名称 FLIGHT ASSISTING DEVICE AND METHOD THEREOF, AND AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To assist a flight while always maintaining communication between an orbiting satellite communication device mounted on an aircraft and an orbiting satellite group. SOLUTION: A flight assisting device includes: an inertial navigation system 4 and a magnetic compass 5 which detect the attitude and azimuth of an aircraft body; a GPS communication device 3 which detects the position of the aircraft body; an orbiting satellite orbit arithmetic circuit 12 which detects an orbit of at least one orbiting satellite having a communication line established with the orbiting satellite communication device 2 in the orbiting satellite group; an antenna pattern that the orbiting satellite communication device 2 has and wherein a communicable range of an orbiting antenna is registered; a movable area calculating arithmetic circuit 14 which calculates a movable area wherein the aircraft can move while maintaining the communication line established between the orbiting satellite communication device 2 and orbiting satellite group based upon the orbit of the orbiting satellite, the antenna pattern, the position of the aircraft body, and the attitude and azimuth; and a display device 16 which reports the movable area to a pilot of the aircraft. COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2008011152(A) 申请公布日期 2008.01.17
申请号 JP20060179325 申请日期 2006.06.29
申请人 MITSUBISHI HEAVY IND LTD 发明人 MIYANISHI IPPEI;HIRANUMA SATOSHI;SHINNOU YUUICHIROU
分类号 H04B7/26;B64D45/00;H04B7/185 主分类号 H04B7/26
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