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42020 年内两个发射窗口的优化结果 |
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| Table 4Optimization results of two launch windows in 2020 |
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