A New Optimal Guidance Law

Author

Xianwei, Zeng ; Yangwang, Fang ; Youli, Wu ; Hongqiang, Wang ; Jiacong, Liu

Author_Institution

Air Force Eng. Univ., Xi´´an

fYear

2007

Firstpage

771

Lastpage

774

Abstract

Based on multisensor information fusion theory and optimal control theory of structure stochastic jump system, a new guidance law is proposed for air-to-air missiles based on information fusion of active radar and infrared sensor, and its validity is testified by analysis on simulation by building digital model of missiles. Compared with proportion navigation law and extended proportion navigation law based on radar or infrared through many Monte Carlo simulations, the results show that the new guidance law reduces errors of tracking target and has smooth trajectory and small over-load, and it is important to theory and engineering application.

Keywords

military radar; missile guidance; sensor fusion; stochastic systems; target tracking; Monte Carlo simulation; active radar; air-to-air missile; infrared sensor; missile digital model; multisensor information fusion; optimal control; optimal guidance law; proportion navigation law; smooth trajectory; stochastic jump system; target tracking; Analytical models; Information analysis; Infrared sensors; Missiles; Navigation; Optimal control; Radar theory; Radar tracking; Stochastic systems; System testing; Extended proportion navigation; Multisensor information fusion; Optimal control; Proportion navigation; Structure stochastic jump system;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference, 2007. CCC 2007. Chinese

Conference_Location

Hunan

Print_ISBN

978-7-81124-055-9

Electronic_ISBN

978-7-900719-22-5

Type

conf

DOI

10.1109/CHICC.2006.4347045

Filename

4347045