| 运载火箭六自由度仿真原理与实现 |
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| 引用本文： | 胡云中,王广民.运载火箭六自由度仿真原理与实现[J].航天控制,1997(1). |
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| 作者姓名： | 胡云中 王广民 |
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| 作者单位： | 北京航天控制工程研究所!100854 |
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| 摘 要： | 给出了运载火箭六自由度运动数学模型，阐述了六自由度数学仿真的一般原理，重点讨论了其工程实现中的关键技术问题，并以某型号为背景进行了制导精度和控制系统稳定性六自由度仿真试验，验证了仿真方案与技术途径的正确性。
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| 关 键 词： | 运载火箭 仿真 制导 姿态控制 |
Principle and Realization of Six-Degree-of-Freedom Simulation for Launch Vehicle |
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| Hu Yunzhon, Wang Guangmin.Principle and Realization of Six-Degree-of-Freedom Simulation for Launch Vehicle[J].Aerospace Control,1997(1). |
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| Authors: | Hu Yunzhon Wang Guangmin |
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| Institution: | Beijing Aerospace Automatic Control Institute 100854 |
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| Abstract: | In this Paper 6 - DOF motional mathematical models of launch vehicles are giv-en,general principle of 6 - DOF mathematical simulation is elaborated, emphasis is given todiscuss a series of key technical questions in engineering realization. 6 - DOF simulation testsare performed on guidance accuracy and attitude control system stability, taken a certainmodel as background. The correctness of simulation scheme and technical way are verificated. |
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| Keywords: | Launch vehicle Simulation guidance Attitude control |
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