敏捷导弹的末制导系统性能综合分析

季登高; 黄兴李; 郭振西

doi:10.15892/j.cnki.djzdxb.2012.04.044

弹箭与制导学报 >

2012 , Vol. 32 >Issue 4: 80 - 83,88

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.04.044

导弹与制导技术

敏捷导弹的末制导系统性能综合分析

季登高 ,
黄兴李 ,
郭振西

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北京临近空间飞行器系统工程研究所,北京 100076

季登高(1981-),男,江苏南通人,工程师,博士,研究方向:飞行器制导与控制、精确末制导相关技术。

收稿日期: 2011-08-31

网络出版日期: 2025-05-29

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Comprehensive Analysis of Terminal Guidance System for Agile Missile

JI Denggao ,
HUANG Xingli ,
GUO Zhenxi

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Beijing Institute of Nearspace Vehicles Systems Engineering, Beijing 100076, China

Received date: 2011-08-31

Online published: 2025-05-29

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摘要

分析末制导系统的有限时间稳定性以及末制导的需用过载,建立末制导回路动态品质与系统性能之间的关系,并讨论直接力的引入时机问题,最后对敏捷导弹的末制导精度进行分析,得到脫靶量、飞行控制系统性能、探测系统性能、量测噪声以及目标机动的关系,结果表明敏捷导弹对探测系统的性能提出了更高的要求。

关键词： 末制导; 敏捷导弹; 性能分析; 有限时间; 脱靶量; 需用过载

本文引用格式

季登高 , 黄兴李 , 郭振西 . 敏捷导弹的末制导系统性能综合分析[J]. 弹箭与制导学报, 2012 , 32(4) : 80 -83,88 . DOI: 10.15892/j.cnki.djzdxb.2012.04.044

Abstract

The finite-time stability and required overload in terminal guidance phase analyzed. The relation between terminal guidance dynamics and system performance established. Based on this, the occasion of introduction for the direct force discussed. By analyzing the terminal guidance precision, the relations miss distance, control system performance, detective system performance, measure noise and target maneuver shown up. The results show that agile missile has higher requirements on the detective system performance.

Key words： derminal guidance; agile missile; performance analysis; finite-time; miss distance; required overload

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参考文献

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[4]	李玉林, 万自明. 直接力/气动力复合控制拦截弹末制导精度研究. 现代防御技术, 2008, 36 (2): 55- 60.
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[6]	季登高. 基于有限时间范数的末制导系统性能分析[D]. 哈尔滨: 哈尔滨工业大学, 2008.
[7]	Denggao Ji, Fenghua He, Yu Yao. Finite time L1 approach for missile overload requirement analysis in terminal guidance[J]. Chinese Journal of Aeronautics, 2009, 22 (4): 413- 418.

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