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)
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) |
| 王艺睿, 李明涛, 周炳红 |
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IMPULSIVE TRAJECTORY OPTIMIZATION OF KINETIC IMPACTOR MISSIONS FOR ASTEROID DEFLECTION BASED ON AN APPROXIMATION DEFLECTION MODEL1) |
| Wang Yirui, Li Mingtao, Zhou Binghong |
| 图6 动能撞击任务流程 |
| Fig. 6 Process of a kinetic impactor mission |
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