日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
固有構造の存在範囲を指定したロバスト飛行制御系の設計
得竹 浩
著者情報
ジャーナル フリー

2001 年 49 巻 573 号 p. 327-333

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抄録

Although the H control method is powerful tool to design robust controller, it is difficult to attain the performances in time domain. A new design method of H state feedback controller is proposed which guarantees the robust stability and assigns eigenstructure in the desired regions. The time responses can be shaped with assigning appropriate eigenstructure. Conditions of robust stability and closed-loop eigenstructure assignments are solved in LMI form with one nonlinear constraint. This method is validated with numerical example of flight control design.

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© 2001 The Japan Society for Aeronautical and Space Sciences
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