2002年
線形補間ゲインスケジューリングを用いた無人宇宙往還機の飛行制御系設計
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
- ,
- ,
- 巻
- 50
- 号
- 582
- 開始ページ
- 278
- 終了ページ
- 285
- 記述言語
- 日本語
- 掲載種別
- DOI
- 10.2322/jjsass.50.278
- 出版者・発行元
- 一般社団法人 日本航空宇宙学会
This paper presents flight control designs of an unmanned space vehicle, HOPE-X, vehicle using interpolation gain scheduling techniques. There are three flight phases from deorbit to landing in HOPE-X; reentry, terminal area energy management (TAEM), and approach and landing. This paper is addressed to the TAEM phase in which an amount of lateral maneuvers are required. Two interpolation gain scheduled state feedback laws were designed with respect to the Lyapunov functions used for guaranteeing the global stability of the closed-loop system, and were applied to the numerical simulations of the HOPE-X. As a result, the gain scheduled control law showed better control performance in the entire of TAEM phase than fixed state feedback laws. The gain scheduling using a parameter-dependent Lyapunov function was superior to the one using a conventional Lyapunov function.
- リンク情報
- ID情報
-
- DOI : 10.2322/jjsass.50.278
- ISSN : 1344-6460
- CiNii Articles ID : 10008967899
- CiNii Books ID : AA11307372