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
相关论文
共 53 条
  • [1] Ammar G., 1991, COMMUNICATIONS CONTR, V338, P163
  • [2] Arita S, 2013, AIAA GUIDANCE NAVIGA, P2013, DOI [10.2514/6.2013-4785, DOI 10.2514/6.2013-4785]
  • [3] Ba s ar T., 1999, Dynamic Noncooperative Game Theory
  • [4] Balakrishnan SN, 2001, P AMER CONTR CONF, P3352, DOI 10.1109/ACC.2001.946146
  • [5] H-INFINITY CONTROL FOR NONLINEAR PLANTS - CONNECTIONS WITH DIFFERENTIAL-GAMES
    BALL, JA
    HELTON, JW
    [J]. PROCEEDINGS OF THE 28TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-3, 1989, : 956 - 962
  • [6] Bardhan R, 2012, P AMER CONTR CONF, P4613
  • [7] Basar T., 1991, OPTIMAL CONTROL RELA
  • [8] Ben-Asher J. Z., 1998, Advances in Missile Guidance Theory, Progress in Astronautics and Aeronautics, V180, P25
  • [9] Optimal Impact Angle Control Guidance Law Based on Linearization About Collision Triangle
    Cho, Hangju
    Ryoo, Chang-Kyung
    Tsourdos, Antonios
    White, Brian
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2014, 37 (03) : 958 - 964
  • [10] Survey of State-Dependent Riccati Equation in Nonlinear Optimal Feedback Control Synthesis
    Cimen, Tayfun
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2012, 35 (04) : 1025 - 1047