NSSC OpenIR  > 空间技术部
Alternative TitleMethod of Mission Analysis for Solar Sail Exploration Based on STK
钱航; 郑建华; 吴霞; 高东; 刘宇飞
Source Publication空间控制技术与应用
Keyword复杂轨道设计 卫星工具包 太阳帆 小推力控制
Abstract研究太阳帆的力学特性和轨道控制设计方法,导出太阳帆的无奇点控制律.提出通过STK中MATLAB语言编写的嵌入式脚本(Plug-in Script)来将由控制律得到的光压力加速度矢量,添加到STK轨道计算力学模型中,从而进行轨道控制的方法.仿真结果表明,对于常规方法难以进行仿真分析的航天器动力学模型(如太阳帆),所提出的方法能快速灵活地支持其相应的任务,并增强任务场景的可视化,从而实现利用STK丰富的功能特性进行复杂航天任务的设计、分析和验证.
Other AbstractDynamic of solar sail and method of trajectory design have been analyzed. Then the control forces calculated by the control strategy are added into the STK orbit propagator, which is realized through the STK plug-in coded by MATLAB. The simulation results show that the methods proposed can realize expeditiously and efficiently that STK/MATLAB coordinated work to neatly support control simulation of special force model such as solar sail dynamic, and the abundant capabilities of STK are suitable for designing and analysising the complex space mission.
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Document Type期刊论文
Recommended Citation
GB/T 7714
钱航,郑建华,吴霞,等. 太阳帆推进任务的快速仿真方法[J]. 空间控制技术与应用,2016,42(2):8-13.
APA 钱航,郑建华,吴霞,高东,&刘宇飞.(2016).太阳帆推进任务的快速仿真方法.空间控制技术与应用,42(2),8-13.
MLA 钱航,et al."太阳帆推进任务的快速仿真方法".空间控制技术与应用 42.2(2016):8-13.
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