论文部分内容阅读
Adaptive Angular Velocity Tracking Control of Spacecraft with Dynamic Uncertainties
【机 构】
：
College of Astronautic,Institute of Aerospace System Engineering Shanghai
【出 处】
：
南京航空航天大学学报（英文版）
【发表日期】
：
2004年期
【基金项目】
：
the Innovation Fund of Shanghai Aerospace Science and Technology
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