基于偏转距离近似模型的动能撞击小行星防御任务脉冲轨道优化研究1)
IMPULSIVE TRAJECTORY OPTIMIZATION OF KINETIC IMPACTOR MISSIONS FOR ASTEROID DEFLECTION BASED ON AN APPROXIMATION DEFLECTION MODEL1)
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基于偏转距离近似模型的动能撞击小行星防御任务脉冲轨道优化研究1) |
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| 王艺睿, 李明涛, 周炳红 | |
IMPULSIVE TRAJECTORY OPTIMIZATION OF KINETIC IMPACTOR MISSIONS FOR ASTEROID DEFLECTION BASED ON AN APPROXIMATION DEFLECTION MODEL1) |
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| Wang Yirui, Li Mingtao, Zhou Binghong | |
| 表9在二体模型基础上每次增加一项摄动力 |
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| Table 9Add one perturbation source at a time based on the two-body model |
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