首页 | 本学科首页   官方微博 | 高级检索  
     

红外拦截弹输出反馈制导控制一体化设计
引用本文:常晶,周军,郭建国. 红外拦截弹输出反馈制导控制一体化设计[J]. 宇航学报, 2018, 39(5): 516-523. DOI: 10.3873/j.issn.1000-1328.2018.05.006
作者姓名:常晶  周军  郭建国
作者单位:西北工业大学精确制导与控制研究所, 西安 710072
摘    要:针对采用红外导引头的拦截弹,提出一种基于滑模观测器的制导控制一体化(IGC)控制方法,在导弹的部分状态已知和非匹配不确定性影响下,确保了其高精度拦截效果。首先,由于采用红外导引头的拦截弹的视线(LOS)角速率难以获取,系统将不满足干扰估计的匹配条件,设计了一种新型滑模观测器,通过构造补偿滑模观测器,同时实现导弹的未知状态和干扰的有限时间精确估计。然后,利用未知状态和干扰估计信息,设计反步控制器实现导弹的制导控制一体化,证明了系统的有界稳定。仿真结果表明,本文提出的方法可以获得较小的脱靶量,且对存在的不确定性具有较强的鲁棒性。

关 键 词:制导控制一体化(IGC)  输出反馈  非匹配不确定性  滑模观测器(SMO)  反步法  
收稿时间:2017-09-08

An Integrated Design of Output Feedback Guidance and Control for the Interceptor with Infrared Seeker
CHANG Jing,ZHOU Jun,GUO Jian guo. An Integrated Design of Output Feedback Guidance and Control for the Interceptor with Infrared Seeker[J]. Journal of Astronautics, 2018, 39(5): 516-523. DOI: 10.3873/j.issn.1000-1328.2018.05.006
Authors:CHANG Jing  ZHOU Jun  GUO Jian guo
Affiliation:Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi’an 710072, China
Abstract:Based on the sliding mode observer, a method for designing an integrated guidance and control (IGC) law is proposed for a class of interceptors which are equipped with infrared seekers and subjected to the unmatched uncertainties. Since the line-of-sight (LOS) rate is difficult to be measured for an interceptor equipped with an infrared seeker and the IGC systems can not satisfy the common matching conditions required for the disturbance estimation, a novel sliding mode observer is constructed by using a compensated observer to estimate the unknown LOS rate and uncertainties in finite time. With the estimated state and uncertainties, the IGC design based on the back-stepping techniques is proposed to achieve the robust tracking of a maneuvering target, even if the interceptor contains uncertainties and is subjected to disturbances. The stability analysis of the closed-loop system is also conducted. Numerical simulations demonstrate the effectiveness of the approach proposed.
Keywords:Integrated guidance and control (IGC)  Output feedback  Unmatched uncertainty;Sliding mode observer (SMO);Back stepping technique  
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号