| 直接力／气动力复合控制防空导弹脱靶量仿真 |
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| 引用本文： | 朱隆魁,汤国建,余梦伦.直接力／气动力复合控制防空导弹脱靶量仿真[J].系统仿真学报,2008,20(23):6563-6565,6568. |
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| 作者姓名： | 朱隆魁 汤国建 余梦伦 |
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| 作者单位： | 国防科技大学航天与材料工程学院，中国航天科技集团公司 |
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| 基金项目： | 国家高技术研究发展计划
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| 摘 要： | 针对力矩式直接力/气动力复合控制防空导弹,给出一种姿控固体小火箭的点火条件和末端修正制导策略,并通过仿真计算研究了对不同运动特性目标的拦截能力以及主要误差因素对终端脱靶量的影响。结果表明该复合控制方法具有很强的弹道修正能力,能在较大空域内实现直接碰撞,但是受雷达导引头测量误差影响十分显著。
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| 关 键 词： | 复合控制 点火条件 末端修正制导 脱靶量 仿真 |
Miss Distance Simulation for Air Defense Missile by Combined Control of Lateral Thrust and Aerodynamic Force |
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| ZHU Long-kui,TANG Guo-jian,YU Meng-lun.Miss Distance Simulation for Air Defense Missile by Combined Control of Lateral Thrust and Aerodynamic Force[J].Journal of System Simulation,2008,20(23):6563-6565,6568. |
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| Authors: | ZHU Long-kui TANG Guo-jian YU Meng-lun |
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| Institution: | ZHU Long-kui1,TANG Guo-jian1,YU Meng-lun2 |
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| Abstract: | An ignition law of lateral pulse rockets and guidance policy of terminal correction was given for air defense missile by combined control of lateral thrust and aerodynamic force.By final miss distance simulation,the interceptibility according to the targets with different motion characteristics was studied and the influence of main error factors was analyzed.The results show that this combined control method has perfect ballistic correction ability,but it is greatly affected by the measurement error of radar seeker. |
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| Keywords: | combined control ignition law terminal correction guidance miss distance simulation |
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