NSSC OpenIR  > 空间技术部
基于轨道动力学的航天器轨道改进方法
Alternative TitleSpacecrafts Orbit Improvement Based-on Orbital Dynamics
周敬
Thesis Advisor郑建华 ; 李明涛
2017
Degree Grantor中国科学院国家空间科学中心
Degree Discipline飞行器设计
Department空间技术部
Keyword轨道改进 轨道动力学 伪相对运动 误差中和 傅里叶变换 曲线拟合
Language中文
Document Type学位论文
Identifierhttp://ir.nssc.ac.cn/handle/122/5895
Collection空间技术部
Recommended Citation
GB/T 7714
周敬. 基于轨道动力学的航天器轨道改进方法[D]. 中国科学院国家空间科学中心,2017.
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2017thesis037.pdf(2788KB)学位论文 开放获取CC BY-NC-SAApplication Full Text
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