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
  • [21] A Nonlinear Optimal Guidance Law with Terminal Impact Angle Constraint
    She H.
    Yang S.
    Ni H.
    Baier H.
    International Journal of Computational Intelligence Systems, 2011, 4 (6) : 1319 - 1324
  • [22] A Nonlinear Optimal Guidance Law with Terminal Impact Angle Constraint
    She, Haoping
    Yang, Shuxing
    Ni, Hui
    Baier, Horst
    INTERNATIONAL JOURNAL OF COMPUTATIONAL INTELLIGENCE SYSTEMS, 2011, 4 (06) : 1319 - 1324
  • [23] Extended state observer based impact angle constrained guidance law for maneuvering target interception
    Xiong, Shaofeng
    Wang, Weihong
    Song, Siyang
    Wang, Sen
    Lai, Chao
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (14) : 2589 - 2607
  • [24] Impact Angle Constraint Guidance Against Active Defense Target Based on Partial Differential Games
    Xu, Biao
    Xu, Jialuo
    Li, Shuang
    Zhang, Jinpeng
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2024, 2024
  • [25] Nonlinear Suboptimal Guidance Law With Impact Angle Constraint: An SDRE-Based Approach
    Wang, Chunyan
    Dong, Wei
    Wang, Jianan
    Shan, Jiayuan
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2020, 56 (06) : 4831 - 4840
  • [26] Generalized Time-Optimal Impact-Angle-Constrained Interception of Moving Targets
    Gopalan, Akhil
    Ratnoo, Ashwini
    Ghose, Debasish
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2017, 40 (08) : 2115 - 2120
  • [27] A Guidance Law Design with Terminal Impact Angle Constraint Based on Nonlinear Generalized Predictive Control
    Lv, Teng
    Li, Chuanjiang
    Sun, Yanchao
    Ma, Guangfu
    Xiao, Junzi
    2014 2ND INTERNATIONAL CONFERENCE ON SYSTEMS AND INFORMATICS (ICSAI), 2014, : 1 - 5
  • [28] Three Dimensional Impact Angle Constrained Guidance Law using Sliding Mode Control
    Kumar, Shashi Ranjan
    Ghose, Debasish
    2014 AMERICAN CONTROL CONFERENCE (ACC), 2014, : 2474 - 2479
  • [29] Field-of-View Constrained Guidance Law for a Maneuvering Target With Impact Angle Control
    Kim, Hyeong-Geun
    Kim, H. Jin
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2020, 56 (06) : 4974 - 4983
  • [30] FOV constrained guidance law for nonstationary nonmaneuvering target interception with any impact angle
    Singh, Nikhil Kumar
    Hota, Sikha
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2022, 236 (10) : 1947 - 1960