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航天器动力学模型试验验证技术研究进展

丁继锋 韩增尧 马兴瑞

丁继锋, 韩增尧, 马兴瑞. 航天器动力学模型试验验证技术研究进展[J]. 力学进展, 2012, 42(4): 395-405. doi: 10.6052/1000-0992-10-012
引用本文: 丁继锋, 韩增尧, 马兴瑞. 航天器动力学模型试验验证技术研究进展[J]. 力学进展, 2012, 42(4): 395-405. doi: 10.6052/1000-0992-10-012
DING Jifeng, HAN Zengyao, MA Xingrui. RESEARCH EVOLUTION ON THE TEST VERIFICATION OF SPACECRAFT DYNAMIC MODEL[J]. Advances in Mechanics, 2012, 42(4): 395-405. doi: 10.6052/1000-0992-10-012
Citation: DING Jifeng, HAN Zengyao, MA Xingrui. RESEARCH EVOLUTION ON THE TEST VERIFICATION OF SPACECRAFT DYNAMIC MODEL[J]. Advances in Mechanics, 2012, 42(4): 395-405. doi: 10.6052/1000-0992-10-012

航天器动力学模型试验验证技术研究进展

doi: 10.6052/1000-0992-10-012
详细信息
    通讯作者:

    韩增尧

RESEARCH EVOLUTION ON THE TEST VERIFICATION OF SPACECRAFT DYNAMIC MODEL

More Information
    Corresponding author: HAN Zengyao
  • 摘要: 耦合载荷分析是航天器研制过程中的一个重要环节, 能够为航天器结构设计, 地面验证试验条件制定以及批准型号发射提供重要依据, 而精确地得到试验验证的航天器动力学分析模型是开展耦合载荷分析的基础. 对于大型复杂航天器结构系统, 动力学模型的试验验证需要统筹安排初始建模、动力学试验、相关分析和模型修正等工作, 这是一项极具挑战的任务. 本文首先给出了结构动力学模型验证的基本流程, 然后重点讨论动力学试验, 相关分析与模型修正等关键技术, 最后结合工程实际的需求, 提出了今后航天器动力学模型试验验证技术研究的重点.

     

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出版历程
  • 收稿日期:  2011-12-28
  • 修回日期:  2012-04-08
  • 刊出日期:  2012-07-25

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