3408 Matched Filter Theoryを用いた最悪突風応答解析(S87-2 飛翔体のモデリングとシステム同定(2),S87 飛翔体のモデリングとシステム同定)

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概要

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• This paper shows a worst case gust response of a typical airfoil section with a control surface. Matched filter theory is employed in order to compute the worst case gust response. The result is compared with response by a 1-minus-cosine gust which is one of the standard representations of discrete gusts. It is found that the matched filter theory can directly obtain the worst case gust response. Meanwhile parametric study is needed to determine the maximum gust response by the 1-minus-cosine gust, which becomes smaller than the worst case gust response by the MFT.

• 2005-09-18

著者

• 神田 淳

  宇宙航空研究開発機構

関連論文

• 3408 Matched Filter Theoryを用いた最悪突風応答解析(S87-2 飛翔体のモデリングとシステム同定(2),S87 飛翔体のモデリングとシステム同定)
• 舵面を有する翼の最悪突風応答解析

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