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
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;
Conference_Titel :
Information and Automation (ICIA), 2010 IEEE International Conference on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-5701-4
DOI :
10.1109/ICINFA.2010.5512293