DocumentCode
3048599
Title
Mixed strategy guidance based on target maneuver detection
Author
Hua Wen-hua ; Chen Xing-lin
Author_Institution
Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
fYear
2010
fDate
20-23 June 2010
Firstpage
884
Lastpage
889
Abstract
With the general separation theorem consideration, two mixed strategy guidance approaches are presented. All based on the target maneuver detection, one approach mixes two available differential game guidance laws to reduce the effect of the estimation delay; the other incorporates one more proposed modified gain differential game guidance law, which increases the lateral acceleration command for estimation delay and short remaining time consideration. The simulation results show that these two approaches can improve the system performance significantly and the second approach has the best performance.
Keywords
differential games; missile guidance; object detection; estimation delay; lateral acceleration command; mixed strategy guidance system; modified gain differential game guidance law; target maneuver detection; Acceleration; Automation; Delay effects; Delay estimation; Detectors; Equations; Space technology; State estimation; Switches; System performance; differential game; maneuver detection; mixed strategy; terminal guidance;
fLanguage
English
Publisher
ieee
Conference_Titel
Information and Automation (ICIA), 2010 IEEE International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-5701-4
Type
conf
DOI
10.1109/ICINFA.2010.5512293
Filename
5512293
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