Chinese Space Science and Technology
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Jing Wuxing Yang Di Wu Yaohua Huang Jianjun (Harbin Institute of Technology)
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Abstract: Feedback control of attitude maneuvers for a flexible space-craft is studied.A time suboptimal feedback control law is presented.Variable torque levels are adopted for vibration suppression.A numericalexample for a large-angle maneuver is given to illustrate effectivenessof the control law.
Jing Wuxing Yang Di Wu Yaohua Huang Jianjun (Harbin Institute of Technology). TIME SUBOPTIMAL FEEDBACK CONTROL OF FLEXIBLE SPACECRAFT DURING A LARGE ANGLE MANEUVER[J]. Chinese Space Science and Technology.
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https://journal26.magtechjournal.com/kjkxjs/EN/Y1993/V13/I06/1
