Robust control of a spin-stabilized spacecraft via a 1DoF gimbaled-thruster and two reaction wheels

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• 作者：Hamed Kouhi^a ; ^{h_kouhi@aut.ac.ir} ; Mansour Kabganian^a ; ^{kabgan@aut.ac.ir} ; Farhad Fani Saberi^b ; ^{f.sabery@aut.ac.ir} ; Morteza Shahravi^c ; ^{shahravim@yahoo.com}
• 关键词：Impulsive orbital maneuver ; Gimbaled-thruster ; Spin-stabilization ; Reaction wheel ; Thrust vector stabilization ; Worst-case output magnitude ; Disturbance rejection
• 刊名：ISA Transactions
• 出版年：2017
• 出版时间：January 2017
• 年：2017
• 卷：66
• 期：Complete
• 页码：310-324
• 全文大小：4383 K
• 卷排序：66

文摘

New thrusting maneuver system based on combination of a 1DoF gimbaled-thruster, two RWs and spin-stabilization. Full disturbance rejection and thrust vector (spin-axis) stabilization without using the RCS and fuel consumption. Confirmation of the linearized model using worst-case output magnitude technique. Multiobjective optimization of the H∞ and control input magnitude. Investigating the rotational kinetic energy needed for spin-up and spin-down.