自寻的反坦克导弹制导控制系统性能指标体系分析
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摘要
半实物仿真已成为导弹制导控制性能的有效评价方法,确立科学的、合理的评估指标体系是测试与评估工作最基本的基础,也是得出正确评估结论的前提。论文通过分析制导控制系统的功能任务,构建了自寻的反坦克导弹半实物仿真条件下性能指标体系,并根据层次分析法对指标体系的权值进行了研究,得到的评估指标体系科学可靠,便于工程应用,也为半实物仿真条件下自寻的反坦克导弹制导控制系统的试验鉴定提供了依据。
Semi-physical simulation has become an effective evaluation method for missile guidance control performance. Establishing a scientific and reasonable evaluation index system is the most basic basis for testing and evaluation,and is also the premise for obtaining correct evaluation conclusions. By analyzing the functional tasks of the guidance control system,this paper constructs a self-seeking anti-tank missile performance index system under the condition of semi-physical simulation,and studies the weight of the index system according to the analytic hierarchy process. The evaluation index system is scientific and reliable, and is convenient for engineering application. It also provides a basis for the experimental indentification of the self-seeking anti-tank missile guidance control system under semi-physical simulation conditions.
Semi-physical simulation has become an effective evaluation method for missile guidance control performance. Establishing a scientific and reasonable evaluation index system is the most basic basis for testing and evaluation,and is also the premise for obtaining correct evaluation conclusions. By analyzing the functional tasks of the guidance control system,this paper constructs a self-seeking anti-tank missile performance index system under the condition of semi-physical simulation,and studies the weight of the index system according to the analytic hierarchy process. The evaluation index system is scientific and reliable, and is convenient for engineering application. It also provides a basis for the experimental indentification of the self-seeking anti-tank missile guidance control system under semi-physical simulation conditions.
引文
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[2]谭薇,秋实,赵华.导弹制导控制系统性能评价试验研究[J].飞航导弹,2002(2):44-47.
[3]倪汉昌.飞航导弹抗干扰评估模拟试验技术研究[J].飞航导弹,2001(9):45-51.
[4]宋贵宝,吉礼超,刘冬.防空导弹制导系统综合效能评估指标体系研究[J].战术导弹技术,2009,5:011.
[5]汤锦祖,张欣光.高超声速飞行器滑翔再入性能评估[J].火力指挥与控制,2012,37(8):120-123.
[6]任伟,熊鹰,张树龙.基于网络分析法的舰舰导弹性能评估方法研究[J].舰舰电子工程,2012,32(10):26-28.
[7]王永寿.导弹制导控制系统性能的评价方法[J].飞航导弹,2002(9):55-58.
[8]韩英红,邢晓岚,陈万春.空空导弹性能指标体系与评估方法[J].战术导弹技术,2011(3):32-37.
[9]傅若韦,宋执环.控制系统性能评估的研究现状与展望[J].华中科技大学学报,2013:3.
[10]王雨潇.制导控制系统性能评估方法研究[D].哈尔滨:哈尔滨工业大学,2014.
[11] Hanson J. Advanced guidance and control project for reusable lauch vehicles[C]//AIAA Guidance,Navigation and Conrolconfereence and Exhibit,2010:1-10.
[12]王长青,余文学,史晓丽.空天飞行器制导技术展望[J].战术导弹技术,2016(6):1-7.
[13]曾庆华,张为华.无人飞行控制技术与工程[M].北京:国防工业出版社,2011.