Control law design for the energy management phase of a winged re-entry vehicle

Taro Tsukamoto, Masaaki Yanagihara, Yoshikazu Miyazawa, Hitoshi Takatsuka

研究成果: 書籍/レポート タイプへの寄稿会議への寄与

1 被引用数 (Scopus)

抄録

A control law for the terminal area energy management (TAEM) phase of a winged re-entry vehicle was designed. During the TAEM phase, the dynamics of the vehicle vary considerably because of changes of velocity and altitude. In addition, there is a significant error in the measured value of Mach number, which is used as a scheduling parameter. The multiple delay model and multiple design point (MDM/MDP) approach is a practical method of designing a controller that can operate over a large range of flight conditions. In this paper, the MDM/MDP approach is used to design a gain-scheduled controller and the resulting design is verified by linear stability analysis, linear command response, and nonlinear flight simulation.

本文言語英語
ホスト出版物のタイトルGuidance, Navigation, and Control Conference and Exhibit
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ページ593-598
ページ数6
出版ステータス出版済み - 1999
イベントGuidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, 米国
継続期間: 8月 9 19998月 11 1999

その他

その他Guidance, Navigation, and Control Conference and Exhibit, 1999
国/地域米国
CityPortland
Period8/9/998/11/99

!!!All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 制御およびシステム工学
  • 電子工学および電気工学

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