| 便携式防空导弹初始段复合控制的研究 |
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| 引用本文： | 章丽苹,李一波,张晓东,张广利.便携式防空导弹初始段复合控制的研究[J].沈阳航空工业学院学报,2010,27(1):48-51,55. |
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| 作者姓名： | 章丽苹 李一波 张晓东 张广利 |
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| 作者单位： | 1. 沈阳航空工业学院,辽宁,沈阳,110136
2. 沈阳航天新乐有限责任公司,辽宁,沈阳,110034 |
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| 摘 要： | 针对某型便携式导弹，研究了其初始段侧向推力与空气动力的复合控制。首先介绍了自旋导弹控制力产生机理，建立了引入侧向推力后的动力学模型，设计了相应的控制方法，并对其进行了仿真。仿真结果表明引入侧向推力后的控制效果与加前置量的效果相近，可以达到直瞒的目的。
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| 关 键 词： | 便携式防空导弹 侧向推力 复合控制 |
Study on initial segment lateral thrust vector control of portable anti-aircraft missile |
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| ZHANG Li-ping,LI Yi-bo,ZHANG Xiao-dong,ZHANG Guang-li.Study on initial segment lateral thrust vector control of portable anti-aircraft missile[J].Journal of Shenyang Institute of Aeronautical Engineering,2010,27(1):48-51,55. |
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| Authors: | ZHANG Li-ping LI Yi-bo ZHANG Xiao-dong ZHANG Guang-li |
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| Institution: | ZHANG Li - ping LI Yi - bo ZHANG Xiao - dong ZHANG Guang - li (1. Shenyang Institute of Aeronautical Engineering, Liaoning Shenyang 110136 ;2. Shenyang Aerospace Xinle Co. Lto, Liaoning Shenyang 110034 ) |
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| Abstract: | In this paper compound control of lateral thrust and aero - dynamic in initial segment was studied based on certain type of portable missile. At first , it introduces the control mechanism of spinning missile, then establishes the dynamic model with lateral thrust added, and then designes the corresponding control method, at last carries on the simulation. The results verify the effect that after adding lateral thrust control can match the effect with advanced angle, there to achieve the goal of direct aiming. |
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| Keywords: | portable air - defense missile lateral thrust compound control |
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