DocumentCode
3032646
Title
Maneuver target interception based on multiple model adaptive estimator
Author
Hua, Wen-hua ; Chen, Xing-lin ; Wu, Zhi-peng
Author_Institution
Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
fYear
2010
fDate
8-10 June 2010
Firstpage
185
Lastpage
190
Abstract
A maneuver target interception algorithm based on multiple model adaptive estimator (MMAE) is researched and a modified differential game guidance law is given. The efficiency of this simplified MMAE algorithm lies mainly in the exploitation of the special structure of the evader maneuver command hypothesis space to reduce the number of MMAE elemental filters running in parallel and to realize the reduction of the computational load. To realize the reduction of the miss distance resulting from the estimation delay, the modified differential game guidance law increases the lateral acceleration command for small values of time-to-go of the pursuer to the maximum available value by enhancing the gain of the command. The Monte Carlo simulations are carried out for the homing performance comparison and the results demonstrate the superiority and effective of the proposed methods.
Keywords
Monte Carlo methods; adaptive Kalman filters; adaptive estimation; target tracking; MMAE; Monte Carlo simulations; elemental filters; estimation delay; evader maneuver command hypothesis space; maneuver target interception; modified differential game guidance law; multiple model adaptive estimator; Acceleration; Estimation; Filtering theory; Games; Mathematical model; Noise; Switches;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5632563
Filename
5632563
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