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

被引:59
|
作者
Bardhan, Rajarshi [1 ]
Ghose, Debasish [1 ]
机构
[1] Indian Inst Sci, Dept Aerosp Engn, Bangalore 560012, Karnataka, India
关键词
DEPENDENT RICCATI-EQUATION; SLIDING-MODE GUIDANCE; INTEGRATED GUIDANCE; MIDCOURSE GUIDANCE; TERMINAL GUIDANCE; MISSILE GUIDANCE; INTERCEPTION; TARGETS;
D O I
10.2514/1.G000940
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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.
引用
收藏
页码:384 / 402
页数:19
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