Robust Adaptive Variable Structure Control of a Flexible Spacecraft Containing Input Nonlinearity/Dead-Zone
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概要
- 論文の詳細を見る
- 社団法人 日本航空宇宙学会の論文
- 2006-11-04
著者
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Hu Qinglei
Department Of Control Science And Engineering Harbin Institute Of Technology
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Ma Guangfu
Department Of Control Science And Engineering Harbin Institute Of Technology
関連論文
- Maneuvers and Vibration Suppression of Flexible Spacecraft Integrating Variable Structure Control and Input Shaping Technique
- Robust Adaptive Variable Structure Control of a Flexible Spacecraft Containing Input Nonlinearity/Dead-Zone