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基于轨道动力学的航天器轨道改进方法
学位论文
, 基于轨道动力学的航天器轨道改进方法: 中国科学院国家空间科学中心, 2017
Authors:
周敬
Adobe PDF(2788Kb)
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View/Download:109/5
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Submit date:2017/08/29
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
太阳帆航天器的轨道动力学和轨道控制研究
期刊论文
宇航学报, 2009, 卷号: 30, 期号: 6, 页码: 1211-1217
Authors:
罗超
;
郑建华
;
高东
;
北京8701信箱
Adobe PDF(654Kb)
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View/Download:319/193
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Submit date:2014/04/30
太阳帆
轨道动力学
轨道控制