DocumentCode
2001922
Title
Application and Simulation of Kalman Filtering with Anti-Jamming
Author
Xiaobin, Zhou ; Yangwang, Fang ; Yafei, Wang
Author_Institution
Air Force Eng. Univ., Xian
fYear
2007
fDate
May 30 2007-June 1 2007
Firstpage
696
Lastpage
700
Abstract
Classifying the jamming of guidance system and inducing its characteristics; and the importance of jamming and anti-jamming in the missile guidance are analyzed. In order to make the missile dive target with higher speed and attack it in the limited time, designing Kalman filter based on missile and target relative movement modeling; researching the anti-jamming abilities and techniques. The result of simulation shows that it can obtain the anticipative effect under the certain of parameter selection and adjustment and this method has good value of theory and application.
Keywords
Gaussian noise; Kalman filters; jamming; missile guidance; optimal control; simulation; stochastic systems; white noise; Gauss white noise; Kalman filtering; anti-jamming technique; maximum principle; missile guidance system; optimal control; parameter selection; simulation; stochastic system; target relative movement modeling; Amplitude modulation; Analytical models; Filtering; Jamming; Kalman filters; Missiles; Noise level; Pulse modulation; Radar; Weapons; anti-jamming; kalman filter; misslie guidance law; simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation, 2007. ICCA 2007. IEEE International Conference on
Conference_Location
Guangzhou
Print_ISBN
978-1-4244-0818-4
Electronic_ISBN
978-1-4244-0818-4
Type
conf
DOI
10.1109/ICCA.2007.4376444
Filename
4376444
Link To Document