DocumentCode :
2549099
Title :
Research on optimal maneuvering opportunity numerical calculation of ballistic missile based on genetic algorithm
Author :
Jie, Feng ; Yong, Xian ; Ming-Hai, Wang ; Peng-Tao, Wei
Author_Institution :
Res. Inst. of High Technol. in Hong Qing Town, Xi´´an, China
fYear :
2010
fDate :
16-18 April 2010
Firstpage :
434
Lastpage :
438
Abstract :
Optimal maneuvering opportunity calculation of ballistic missile is a complicated optimum programming in nonlinear system which need compute trajectories of maneuvering and interception missiles simultaneity, and the requirement of precision and efficiency can not be ignored, so traditional algorithms such as enumeration and heuristic method can not satisfy the requirement because of the low efficiency and narrow applied extension. On a base of relatively motion equation between both sides and guidance equation of EKV, we designed two kinds of optimization models to calculate maneuvering opportunity separately based on GA. The simulation results indicated that the method is effective.
Keywords :
ballistics; genetic algorithms; missiles; nonlinear systems; ballistic missile numerical calculation; exoatmospheric kill vehicle; genetic algorithm; guidance equation; interception missiles; motion equation; nonlinear system; optimal maneuvering opportunity; optimization models; optimum programming; Acceleration; Computer vision; Design optimization; Difference equations; Differential equations; Genetic algorithms; Missiles; Navigation; Nonlinear systems; Vehicles; coding; exoatmospheric kill vehicle; genetic algorithm; maneuvering opporitunity;
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.2010.5477859
Filename :
5477859
Link To Document :
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