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鈴木, 広一, 外立, 政隆, Suzuki, Hirokazu, Hashidate, Masataka航空宇宙技術研究所1995-11航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory688p.1-24

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Subject Heading飛行シミュレーションプログラム誘導則高高度無人機 HALEUV 空力特性レクテナ翼マイクロ波伝送装置運動方程式横方...
Note (General)...anned Vehicle (HALEUV). At first, eq......acteristics of HALEUV are estimated.......f 20 km, which HALEUV is expected to......ce law for the HALEUV is designed to......icate that the HALEUV can stay withi......m, even if the HALEUV encounters with a strong wind...

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