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 50 条
  • [31] Observer-Based Guidance Law With Impact Angle Constraint
    Qu, Pingping
    Zhou, Di
    Sun, Sheng
    JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2017, 139 (11):
  • [32] Optimal Control Based Guidance Law with Impact Angle Constraint
    Chen, Xiaotian
    Wang, Jinzhi
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 6000 - 6004
  • [33] Quaternion based Three-Dimensional Impact Angle Constrained Guidance
    Surve, Prajakta
    Maity, Arnab
    Kumar, Shashi Ranjan
    IFAC PAPERSONLINE, 2020, 53 (02): : 9446 - 9451
  • [34] Trajectory Correcting and Tracking Based Impact Angle Constrained Circular Guidance
    Zeng, Xianfa
    Wang, Jieyao
    Wang, Xiaohu
    2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2014, : 2729 - 2733
  • [35] A 3D Nonlinear Guidance Law with Impact Terminal Angle Constraints
    Li Xinsan
    Wang Lixin
    Chen Ke
    Yan Xunliang
    Fan Xiaohu
    Ding Bangping
    2015 CHINESE AUTOMATION CONGRESS (CAC), 2015, : 2242 - 2246
  • [36] Fractional Order Differential Sliding Mode Guidance Law with Impact Angle Constraint
    Xia, Lei
    Sheng, Yongzhi
    2023 35TH CHINESE CONTROL AND DECISION CONFERENCE, CCDC, 2023, : 2227 - 2233
  • [37] Three-dimensional impact angle constrained nonlinear guidance with predefined convergence time
    Majumder, Kakoli
    Kumar, Shashi Ranjan
    NONLINEAR DYNAMICS, 2024, 112 (12) : 9983 - 10008
  • [38] Look Angle Constrained Impact Angle Control Guidance Law for Homing Missiles With Bearings-Only Measurements
    Kim, Hyeong-Geun
    Lee, Jun-Yong
    Kim, H. Jin
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2018, 54 (06) : 3096 - 3107
  • [39] Guidance law with impact angle and impact time constraints
    An, Binghe
    Wang, Yongji
    Liu, Lei
    PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 8260 - 8264
  • [40] Guidance law with impact time and impact angle constraints
    Zhang Youan
    Ma Guoxin
    Liu Aili
    Chinese Journal of Aeronautics, 2013, 26 (04) : 960 - 966