| 航天器热模型蒙特卡罗法修正论述 |
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| 引用本文： | 杨沪宁,钟奇.航天器热模型蒙特卡罗法修正论述[J].航天器工程,2009,18(3):53-58. |
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| 作者姓名： | 杨沪宁 钟奇 |
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| 作者单位： | 北京空间飞行器总体设计部,北京,100094 |
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| 摘 要： | 对近年来国外应用较多的航天器热模型蒙特卡罗修正法进行了分析和介绍;引入了航天器热模型修正的反问题理论,给出了基于蒙特卡罗法的反演解算方法。在Thermal Desktop+Sinda Fluint软件平台上实现了该算法,分析结果表明此方法无需人工干预,可以得出较好的反演效果,适合于在今后的航天器热模型修正工作中开展应用。
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| 关 键 词： | 航天器 热模型 蒙特卡罗 模型修正 |
Monte-Carlo Method for Thermal Model Correction of Spacecraft |
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| YANG Huning,ZHONG Qi.Monte-Carlo Method for Thermal Model Correction of Spacecraft[J].Spacecraft Engineering,2009,18(3):53-58. |
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| Authors: | YANG Huning ZHONG Qi |
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| Institution: | Beijing Institute of Spacecraft System Engineering;Beijing 100094;China |
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| Abstract: | This paper introduces and analyzes Monte-Carlo(MC) technique for thermal model correction of spacecraft. An inverse problem of spacecraft model is developed,which is solved with MC scenario.A practical example is given to correct stochastic parameters on MC method with ThermalDesktop+SindaFluint software. The computational results show that the MC scenario is effective for correcting parameters and demands less manpower. The results can be used to instruct the follow-on engineering design. |
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| Keywords: | spacecraft thermal model Monte-Carlo technique parameter correction |
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