DocumentCode
2897414
Title
Capturability of Augmented Proportional Navigation (APN) guidance with nonlinear engagement dynamics
Author
Ghosh, Sudip ; Ghose, Debasish ; Raha, Soumyendu
Author_Institution
IISc Math. Initiative, Indian Inst. of Sci., Bangalore, India
fYear
2013
fDate
17-19 June 2013
Firstpage
7
Lastpage
12
Abstract
Proportional Navigation (PN) and its variants are widely used guidance philosophies. However, in the presence of target maneuver, PN guidance law is effective only for a restrictive set of initial geometries. To account for target maneuvers, the concept of Augmented Proportional Navigation (APN) guidance law was introduced and analyzed in a linearized interceptor-target engagement framework presented in literature. However, there is no work in the literature, that addresses the capturability performance of the APN guidance law in a nonlinear engagement framework. This paper presents such an analysis and obtains the conditions for capturability. It also shows that a shorter time of interception is obtained when APN is formulated in the nonlinear framework as proposed in this paper. Simulation results are given to support the theoretical findings.
Keywords
aircraft navigation; linearisation techniques; motion control; nonlinear control systems; nonlinear dynamical systems; proportional control; target tracking; APN guidance law; augmented proportional navigation; capturability performance; guidance philosophies; linearized interceptor-target engagement framework; nonlinear engagement dynamics; nonlinear engagement framework; target maneuver; Acceleration; Aerospace engineering; Control systems; Equations; Geometry; Laboratories; Navigation;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2013
Conference_Location
Washington, DC
ISSN
0743-1619
Print_ISBN
978-1-4799-0177-7
Type
conf
DOI
10.1109/ACC.2013.6579805
Filename
6579805
Link To Document