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航天器相对运动与Hill解的适用性分析 期刊论文
中国空间科学技术, 2002, 卷号: 22, 期号: 2, 页码: 1-8
Authors:  张振民;  许滨;  张珩;  孙兰;  潘力均
Adobe PDF(397Kb)  |  Favorite  |  View/Download:352/107  |  Submit date:2010/05/03
动力学方程  相对运动  适应条件  航天器  
Analysis of Spacecraft Relative Motion and Applicability of Hill's Solution 期刊论文
Chinese Space Science and Technology, 2002, 期号: 2, 页码: 1-8
Authors:  Zhang ZM(张振民);  Xu B(许滨);  Zhang H(张珩);  Sun L(孙兰);  Pan LJ(潘力均)
Adobe PDF(245Kb)  |  Favorite  |  View/Download:455/129  |  Submit date:2007/06/15
An analytical approach to analyzing spacecraft formation-flying motion 会议论文
AIAA Guidance, Navigation, and Control Conference and Exhibit 2002, Monterey, CA, United states, August 5, 2002 - August 8, 2002
Authors:  Zhang H(张珩);  Xu B(许滨);  Zhang ZM
View  |  Adobe PDF(248Kb)  |  Favorite  |  View/Download:22/8  |  Submit date:2017/06/01
Analytical Approach  Flight Trajectory  Formation Flying  Reference Spacecraft  Relative Motion  Simplified Formula