スペース・エンジニアリング・コンファレンス講演論文集
Online ISSN : 2424-3191
ISSN-L : 0918-9238
セッションID: F2
会議情報
F2 準軌道型宇宙輸送システムの開発計画と飛行実験(設計・開発手法)
米本 浩一
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会議録・要旨集 フリー

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The Space Systems Laboratory of Kyushu Institute of Technology has been studying unmanned suborbital winged rocket as a research subject of future fully reusable space transportation system since 2005. The flight tests of a small scaled winged rocket were conducted five times from 2008 to 2009. A larger winged rocket with a hybrid called CAMUI, which will reach to a higher altitude, is under development in collaboration with Hokkaido University, National Defense Academy, JAXA, IHI Aerospace Co. Ltd., and other aerospace industries for validating INS/GPS hybrid navigation system, real time trajectory generation and guidance algorithm using GA implemented on FPGA, H∞ and adaption control theory. This paper reports current design, development and flight test plan of the winged rocket.
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© 2011 一般社団法人 日本機械学会
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