| 一种高精度在轨试验窗口设计方法研究 |
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| 引用本文： | 王征.一种高精度在轨试验窗口设计方法研究[J].导弹与航天运载技术,2020(2):23-27. |
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| 作者姓名： | 王征 |
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| 作者单位： | 中国运载火箭技术研究院 |
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| 摘 要： | 在空间试验任务中,合理的试验窗口规划是保障飞行任务顺利开展的前提。考虑试验过程中的地面测控约束、可见光相机光照约束、太阳高度角极性约束及飞行器本体阳光反射角约束,建立了飞行器高精度轨道动力学模型、在轨试验约束条件模型;利用数学仿真验证了在轨试验窗口设计方法的正确性。
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| 关 键 词： | 地面测控 光照约束 反射角 试验窗口 |
Research on High-precision on-orbit Test Window Calculation Method |
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| Wang Zheng.Research on High-precision on-orbit Test Window Calculation Method[J].Missiles and Space Vehicles,2020(2):23-27. |
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| Authors: | Wang Zheng |
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| Affiliation: | (China Academy of Launch Vehicle Technology,Beijing,100076) |
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| Abstract: | In space missions,propriate On-orbit Test Window is the guarantee for the mission.Considered the Ground Tracking System’s constraint,Visible Light Camera’s lighting constraint,Solar elevation angle’s constraint and the Flying Vehicle’s reflection angle constraint,the orbital dynamic model and the on-orbit test constraints’calculation model have been established,while the trial is carrying out.The effectiveness of Multi-constraints On-orbit Test Window Calculation Method is verified by mathematical simulation. |
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| Keywords: | ground tracking lighting constraint reflection angle on-orbit test window |
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