多约束制导律与导引头隔离度制导匹配性研究

doi:10.3969/j.issn.1000-1093.2015.08.014

兵工学报 ›› 2015, Vol. 36 ›› Issue (8): 1473-1480.doi: 10.3969/j.issn.1000-1093.2015.08.014

多约束制导律与导引头隔离度制导匹配性研究

张文渊¹，夏群利¹，刘大卫²

(1.北京理工大学宇航学院，北京 100081; 2.中国兵器科学研究院，北京 100089)

收稿日期:2014-12-09 修回日期:2014-12-09 上线日期:2015-10-16
通讯作者: 张文渊 E-mail:zhwy_bit@163.com
作者简介:张文渊（1987—），男，博士研究生
基金资助:
国家科技重大专项（2013年）

Research on Guidance Matching of Guidance Law with Multiple Constraints and Seeker Disturbance Rejection Rate

ZHANG Wen-yuan¹, XIA Qun-li¹, LIU Da-wei²

(1.School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;2Ordnance Science and Research Academy of China, Beijing 100089, China)

Received:2014-12-09 Revised:2014-12-09 Online:2015-10-16
Contact: ZHANG Wen-yuan E-mail:zhwy_bit@163.com

摘要/Abstract

摘要： 针对导引头隔离度影响多约束制导系统稳定性与制导精度的问题，推导了一种多约束制导律（GLMC），在此基础上构建了考虑导引头隔离度的多约束制导模型。研究了导引头隔离度和制导参数等对制导系统稳定性的影响规律，采用伴随函数法，分析了有无导引头隔离度影响情况下GLMC制导性能变化规律。结果表明，减小制导时间常数、增大隔离度幅值，以及剩余飞行时间的减小都会降低系统稳定性。GLMC能容忍的隔离度水平大约为1%，在实际工程应用中，要保证GLMC较为先进的制导性能，需严格控制导引头的隔离度水平，降低寄生回路对制导系统稳定性的影响。

关键词: 兵器科学与技术, 多约束制导律, 制导稳定性, 寄生回路, 导引头隔离度

Abstract: A guidance law with multiple constraints (GLMC) is derived in light of the effect of disturbance rejection rate of seeker on the stability and guidance accuracy of the multi-constraint guidance system, and a multi-constraint guidance model is established, in which the disturbance rejection rate of seeker is considered. The effect of disturbance rejection rate and guidance parameters on the stability of guidance system is analyzed. In addition, the adjoint function is employed to analyze the guidance performance variations of the multi-constraint guidance law with or without the influence of disturbance rejection rate of seeker. The results indicate that any decrease in guidance time constant or flight remaining time as well as increase in the disturbance rejection rate will lead to a decrease in the stability of guidance system. The GLMC can sustain a disturbance rejection rate of about 1%. In the practical applications, it is essential to control the level of disturbance rejection rate of seeker strictly and reduce the effect of parasitical loop on the stability of guidance system so that a superior guidance performance of the multi-constraint guidance law can be ensured.

Key words: ordnance science and technology, guidance law with multiple constraints, guidance stability, parasitic loop, disturbance rejection rate of seeker

中图分类号:

V448.133

张文渊，夏群利，刘大卫. 多约束制导律与导引头隔离度制导匹配性研究[J]. 兵工学报, 2015, 36(8): 1473-1480.

ZHANG Wen-yuan, XIA Qun-li, LIU Da-wei. Research on Guidance Matching of Guidance Law with Multiple Constraints and Seeker Disturbance Rejection Rate[J]. Acta Armamentarii, 2015, 36(8): 1473-1480.

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多约束制导律与导引头隔离度制导匹配性研究

Research on Guidance Matching of Guidance Law with Multiple Constraints and Seeker Disturbance Rejection Rate

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