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
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;
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
DOI :
10.1109/ICIME.2010.5477588