Model independent near eigenaxis rotation for spacecraft maneuver under slew rate and control constraints

被引：0
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作者：
Cao, Xi-Bin [1 ]
Wang, Feng [1 ]
Zhang, Shi-Jie [1 ]
机构：
[1] Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China
来源：
Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology | 2006年 / 38卷 / 09期
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页码：1413 / 1418
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