| 倾斜零长发射技术研究 |
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| 引用本文： | 张胜三,顾银芳. 倾斜零长发射技术研究[J]. 导弹与航天运载技术, 2009, 0(6) |
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| 作者姓名： | 张胜三 顾银芳 |
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| 作者单位： | 北京航天发射技术研究所,北京,100076 |
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| 摘 要： | 利用虚拟样机技术(VPT)建立了飞行器零长发射过程的动力学仿真模型.详细论述了飞行器发射系统的组成、模型简化和动力学仿真的研究方法.对不同工况下的发射过程进行动力学分析,获取了飞行器发射阶段的姿态参数和发射车的稳定性,验证了飞行器零长发射的可行性和安全性.
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| 关 键 词： | 飞行器 倾斜零长发射 虚拟样机技术 仿真 |
Research of Oblique Zero-length Launching Technology |
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| Zhang Shengsan,Gu Yinfang. Research of Oblique Zero-length Launching Technology[J]. Missiles and Space Vehicles, 2009, 0(6) |
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| Authors: | Zhang Shengsan Gu Yinfang |
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| Abstract: | Dynamic simulation model in zero-length launching of the vehicle is achieved by the virtual prototype technology (VPT).Composition,model simplification and dynamic simulation of zero-length launching are discussed.Dynamic analyses in launching under different operating states age done.Attitude parameters during launching of the vehicle and the stability of the launcher are obtained.Feasibility and safety in zero-length launching of the the vehicle are verified. |
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| Keywords: | Vehicle Oblique zero-length launching Virtual prototype technology Simulation |
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