| 中远距空空导弹制导控制系统建模与仿真研究 |
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| 引用本文： | 宋龙,任章. 中远距空空导弹制导控制系统建模与仿真研究[J]. 弹箭与制导学报, 2006, 26(4): 1-6 |
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| 作者姓名： | 宋龙 任章 |
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| 作者单位： | 1. 中国空空导弹研究院,河南洛阳,471009;北京航空航天大学,北京,100083
2. 北京航空航天大学,北京,100083 |
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| 摘 要： | 文中首先建立了中远距空空导弹的六自由度的制导控制系统的数学模型．并根据包括飞行试验的各种半实物仿真试验的结果对模型进行了修订，然后编制了以C语言为基础的模块化设计的仿真软件。给出了仿真算例。仿真结果表明．与实际飞行试验数据达到非常好的拟合，说明采用六自由度的制导控制系统的数学模型进行设计的正确性。
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| 关 键 词： | 中远距空空导弹 制导 控制 建模 仿真 |
| 收稿时间： | 2006-04-07 |
| 修稿时间： | 2006-04-07 |
Study on Modeling and Simulation of Medium Range Air-to-air Missile Guidance System |
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| SONG Long,REN Zhang. Study on Modeling and Simulation of Medium Range Air-to-air Missile Guidance System[J]. Journal of Projectiles Rockets Missiles and Guidance, 2006, 26(4): 1-6 |
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| Authors: | SONG Long REN Zhang |
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| Affiliation: | 1.China Airborne Missile Academy, Henan Luoyang 471009, China; 2.Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | In this paper, we first establish the mathematics model of six-degrees-freedom guidance-control system model of medium range air-to-air missile. And the model has been validated by the various hardware-in-loop simulation results including flight test results, Then the simulation software using the modularization design method based on C language is written. Numerical simulation results for sample engagement scenarios are given. It shows that simulation results are very close to the actual flight test results. So these design approaches using a six-degrees-freedom medium range air-to air missile model are accurate. |
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| Keywords: | medium range air-to-air missile guidance control modeling simulation |
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