载人小行星探测目标选择与轨道优化设计

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1.
bob手机在线登陆深空探测技术研究所,北京100081;飞行器动力学与控制教育部重点实验室,北京100082
2.
bob手机在线登陆深空探测技术研究所,北京100081;飞行器动力学与控制教育部重点实验室,北京100083
3.
bob手机在线登陆深空探测技术研究所,北京100081;飞行器动力学与控制教育部重点实验室,北京100084
4.
bob手机在线登陆深空探测技术研究所,北京100081;飞行器动力学与控制教育部重点实验室,北京100085

基金项目:国家重点基础研究发展计划(973计划)(2012CB720000)；国家自然科学基金资助项目（11101021)；bob手机在线登陆创新团队基金资助项目

Target Selection and Trajectory Design for Manned Asteroid Missions

1.
Institute of Deep Space Exploration Technology, Beijing Institute of Technology, Beijing 100081,China;Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100082,China
2.
Institute of Deep Space Exploration Technology, Beijing Institute of Technology, Beijing 100081,China;Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100083,China
3.
Institute of Deep Space Exploration Technology, Beijing Institute of Technology, Beijing 100081,China;Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100084,China
4.
Institute of Deep Space Exploration Technology, Beijing Institute of Technology, Beijing 100081,China;Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100085,China

摘要:针对2020 - 2040年载人小行星探测任务，研究了探测目标选择与轨道优化设计问题。首先，针对已编目的近地小行星，综合考虑绝对星等、燃料消耗等多方面因素与约束，给出了适合载人探测任务的候选小行星序列;然后，构建了载人小行星探测任务轨道的设计模型，采用参数优化算法对探测轨道进行了设计;进一步，为了获得最优探测轨道，利用主矢量原理对探测轨道进行了优化。该研究可为载人小行星探测任务设计提供有价值的参考。
- 近地小行星/
- 小行星探测/
- 载人探测/
- 目标选择/
- 轨道优化
Abstract:In this paper, the target selection and trajectory optimization is investigated for manned asteroid exploration mission in 2020一2040. Firs街，According to various factors and constraints , such as absolute magnitude and orbital parameters, 20 potential candidates for manned missions are presented. And then, the design model for manned mission is constructed, and the exploration trajectories for asteroid candidates are computed场using parameters optimization algorithm directly. Furthermore, the prime vector theory is used to obtain the optimal exploration trajectories. This research can provide valuable proposals for future manned asteroid missions
- near-earth asteroid/
- asteroid exploration/
- manned exploration/
- target selection/
- trajectory optimization

[1]

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