Flight control law design with hierarchy-structured dynamic inversion approach

Jun Ichiro Kawaguchi, Yoshikazu Miyazawa, Tetsujiro Ninomiya

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

24 被引用数 (Scopus)

抄録

This paper proposes an automatic flight control law design methodology for a trajectory tracking problem by use of hierarchy-structured dynamic inversion approach, which is based on multi-time-scale separation and multi-loop closure method. It considerably simplifies a flight control design compared with the conventional PID approach which is augmented with the gain scheduling technique. It realizes a universal design of the controller which utilizes the vehicle's 6DOF simulation data on board. The dynamic equations employed are categorized into four groups according to their time-scales in a physically natural manner, where the variables in each category are controlled by the faster variables in the adjoining category. In this paper, preliminary evaluation using a linear model is carried out in the first place to ensure the validity of the approach, and a further analysis is conducted with a 6DOF simulation model.

本文言語英語
ホスト出版物のタイトルAIAA Guidance, Navigation and Control Conference and Exhibit
出版社American Institute of Aeronautics and Astronautics Inc.
ISBN(印刷版)9781563479458
DOI
出版ステータス出版済み - 1 1 2008

出版物シリーズ

名前AIAA Guidance, Navigation and Control Conference and Exhibit

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 制御およびシステム工学

フィンガープリント

「Flight control law design with hierarchy-structured dynamic inversion approach」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル