DocumentCode
2543206
Title
Research of cooperation guidance scheme based on multiple missiles engagement
Author
Ye, Jikun ; Lei, Humin ; Wang, Fei ; Li, Jiong
Author_Institution
Dept. of Control Sci. & Eng., Missile Inistitude of Air Force Eng. Univ., Sanyuan, China
fYear
2010
fDate
16-18 April 2010
Firstpage
73
Lastpage
77
Abstract
This paper discusses the development of guidance scheme for multiple missiles co-operation engagement. Firstly, based on the intercept point, the mid-course guidance out of the aerosphere is studied to obtain the shutdown condition. Secondly, using the the linearization of the control model and error feedback loop in the mid-course guidance out of the aerosphere, a new guidance law called ITCG (Impact-Time-Control Guidance) law is analyzed. The new guidance law can be used to guide multiple missiles co-operate to hit the target simultaneously with the desired time. Thirdly, based on the minimum information set theory, the procedure of information interchanging of mulitiple missiles engagement is designed, which solves the problem of communication among missiles in ITCG law. Finally, simulations for the proposed co-operation engagement scheme are conducted to validate the effectiveness, and doable performance.
Keywords
feedback; information theory; linearisation techniques; missile guidance; set theory; cooperation guidance scheme; error feedback loop; impact-time-control guidance; information set theory; multiple missiles cooperation engagement; Acceleration; Control systems; Error correction; Feedback loop; Force control; Linear feedback control systems; Missiles; Optimal control; Tellurium; Velocity control; cooperation; guidance; information set; mid-course; proportional guidance;
fLanguage
English
Publisher
ieee
Conference_Titel
Information Management and Engineering (ICIME), 2010 The 2nd IEEE International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-5263-7
Electronic_ISBN
978-1-4244-5265-1
Type
conf
DOI
10.1109/ICIME.2010.5477588
Filename
5477588
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