DocumentCode
3534198
Title
Three dimensional retro-PN based impact time control for higher speed nonmaneuvering targets
Author
Ghosh, Sudip ; Ghose, Debasish ; Raha, Soumyendu
Author_Institution
IISc Math. Initiative, Indian Inst. of Sci., Bangalore, India
fYear
2013
fDate
10-13 Dec. 2013
Firstpage
4865
Lastpage
4870
Abstract
In the implementation of modern guidance laws, especially in impact time constrained engagement scenario or multiple agent salvo attack scenario, a good estimate of time-to-go is extremely crucial. The most widely used time-to-go estimate range over closing speed has several limitations. Very few work is there in existing literature which actually try to estimate the time-to-go. Most of them are meant for the engagement of lower speed target with a higher speed interceptor. However, in the current defence scenario, targets of higher speed than the interceptor is a reality. This paper first discusses a recursive time-to-go estimation method for three dimensional engagement of a Retro-PN guided interceptor with higher speed non-maneuvering target and then presents a navigation gain scheduling algorithm to achieve the interception at a pre-specified time. The effectiveness of the time-to-go estimation method and the gain scheduling algorithm is justified with simulation results.
Keywords
estimation theory; missile guidance; optimal control; higher speed nonmaneuvering targets; missile guidance laws; multiple agent salvo attack scenario; navigation gain scheduling algorithm; retro-PN guided interceptor; three dimensional retro-PN based impact time control; time-to-go estimation method; Adaptive systems; Estimation; Geometry; Navigation; Simulation; Time factors; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on
Conference_Location
Firenze
ISSN
0743-1546
Print_ISBN
978-1-4673-5714-2
Type
conf
DOI
10.1109/CDC.2013.6760652
Filename
6760652
Link To Document