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
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;
Conference_Titel :
American Control Conference (ACC), 2013
Conference_Location :
Washington, DC
Print_ISBN :
978-1-4799-0177-7
DOI :
10.1109/ACC.2013.6579805