| 拖靶系统飞行动力学模型研究 |
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| 引用本文： | 陈峰.拖靶系统飞行动力学模型研究[J].宇航计测技术,2013,33(2):50. |
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| 作者姓名： | 陈峰 |
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| 作者单位： | 1、中国人民解放军92419部队，辽宁 125106 |
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| 摘 要： | 介绍了拖靶系统的基本组成，阐述了建立拖靶系统飞行动力学模型的意义。分别对拖机、拖靶及拖缆进行了受力分析，建立了数学模型并进行了合理假设和简化，分析了系统主要约束关系，可为拖靶系统设计及仿真研究提供参考。
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| 关 键 词： | 拖靶系统 飞行力学 模型 拖缆 |
Research on the Flight Dynamics Model for Towed Target System |
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| CHEN Feng.Research on the Flight Dynamics Model for Towed Target System[J].Journal of Astronautic Metrology and Measurement,2013,33(2):50. |
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| Authors: | CHEN Feng |
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| Institution: | 1、92419 Unit of PLA,Liaoning 125106 |
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| Abstract: | The basic composition of the towed target system is introduced,and the meaning of constructing the flight dynamics model of towed target system is presented.The load analyses of the towing plane,the towed target and the towlines are carried out separately as well as the mathematics model is established and simplified with practical assumption,and the main restrains are analyzed in order to supply the reference for the design and simulation of the towed target system. |
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| Keywords: | Towed target system Flight mechanics Model Towline |
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