Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law
Data(s) |
2015
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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 |