Semi-Analytical Midcourse Guidance for Coordinated Interception of Multiple Exo-Atmospheric Targets

被引:1
|
作者
Zhang, Guoxu [1 ]
Pang, Bo [1 ]
Wen, Changxuan [1 ]
Song, Xun [2 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Beijing Inst Elect Syst Engn, Beijing 100854, Peoples R China
关键词
SIMULTANEOUS ATTACK; CHALLENGES; MISSILES; LAW;
D O I
10.2514/1.A35659
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The simultaneous interception of multiple exo-atmospheric threat targets can leave no buffer time for the targets and greatly reduces targets' penetration probability. This paper proposes centralized and decentralized two midcourse guidance methods to solve the coordinated interception of multiple exo-atmospheric targets. First, the free-time cooperative interception problem minimizing the total impulses is established, where the nonlinear dynamics of the interceptors and targets, the initial impulse constraints, and the terminal interception constraints are considered. Second, the necessary conditions for the optimal cooperative interception problemare derived and then approximated using higher-orderTaylor expansions, which result in a series of analytical nonlinear equations. Then, the semi-analytical centralized guidance mode is designed to achieve simultaneous interception of targets by directly solving the analytical nonlinear equations. To improve computational efficiency, the decentralized cooperative guidancemode is further proposed by using the developed iterative freezing trajectorymethod, where each interceptor uses information from other interceptors in the previous iteration for prediction and distributed computation. Numerical examples verify the effectiveness and robustness of the proposed two guidance methods. Results show that the computational efficiency of the decentralized guidancemode is more efficient compared with the centralized midcourse guidance mode.
引用
收藏
页码:34 / 47
页数:14
相关论文
共 50 条
  • [1] Noniterative feedback midcourse guidance for exo-atmospheric interception of ballistic targets using virtual impact point steering
    Jo, Byeong-Un
    Ahn, Jaemyung
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 119
  • [2] 3D-Nonlinear Vector Guidance and Exo-Atmospheric Interception
    Gutman, Shaul
    Rubinsky, Sergey
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2015, 51 (04) : 3014 - 3022
  • [3] Optimal midcourse guidance law for the exo-atmospheric interceptor with solid-propellant booster
    Zhao, Shilei
    Chen, Wanchun
    Yang, Liang
    Wang, Minghao
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 127
  • [4] Exo-atmospheric guidance of an accelerating interceptor missile
    Shima, Tal
    Golan, Oded M.
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2012, 349 (02): : 622 - 637
  • [5] Optimal Guidance Law with Impact-Angle Constraint and Acceleration Limit for Exo-Atmospheric Interception
    Zhao, Shilei
    Chen, Wanchun
    Yang, Liang
    AEROSPACE, 2021, 8 (12)
  • [6] Pseudospectral Model Predictive Control for Exo-atmospheric Guidance
    Rahman, Tawfiqur
    Zhou, Hao
    Yang, Liang
    Chen, Wanchun
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2015, 16 (01) : 64 - 76
  • [7] Design of predictive guidance law and stability analysis of guidance system for exo-atmospheric interceptor
    Zhang, Guo-Jiang
    Yang, Bao-Qing
    Yao, Yu
    Dandao Xuebao/Journal of Ballistics, 2010, 22 (02): : 10 - 14
  • [8] Optimal Midcourse Guidance Algorithm for Exoatmospheric Interception Using Analytical Gradients
    Du, Wenhao
    Chen, Wanchun
    Yang, Liang
    Zhou, Hao
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2019, 2019
  • [9] The Design of Predictive Guidance Law and Stability Analysis of Guidance System for Exo-atmospheric Interceptor
    Zhang, Guojiang
    Yang, Baoqing
    Yao, Yu
    2010 8TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA), 2010, : 2383 - 2387
  • [10] Three-dimensional midcourse guidance using neural networks for interception of ballistic targets
    Song, EJ
    Tahk, MJ
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2002, 38 (02) : 404 - 414