Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law


Autoria(s): Bardhan, Rajarshi; Ghose, Debasish
Data(s)

2015

Resumo

The problem of intercepting a maneuvering target at a prespecified impact angle is posed in nonlinear zero-sum differential games framework. A feedback form solution is proposed by extending state-dependent Riccati equation method to nonlinear zero-sum differential games. An analytic solution is obtained for the state-dependent Riccati equation corresponding to the impact-angle-constrained guidance problem. The impact-angle-constrained guidance law is derived using the states line-of-sight rate and projected terminal impact angle error. Local asymptotic stability conditions for the closed-loop system corresponding to these states are studied. Time-to-go estimation is not explicitly required to derive and implement the proposed guidance law. Performance of the proposed guidance law is validated using two-dimensional simulation of the relative nonlinear kinematics as well as a thrust-driven realistic interceptor model.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/52298/1/Jou_of_Gui_Con_and_Dyn_38-3_384_2015.pdf

Bardhan, Rajarshi and Ghose, Debasish (2015) Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law. In: JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 38 (3). pp. 384-402.

Publicador

AMER INST AERONAUTICS ASTRONAUTICS

Relação

http://dx.doi.org/10.2514/1.G000940

http://eprints.iisc.ernet.in/52298/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed