Field-of-View Constrained Impact Time Guidance Against Stationary Targets

被引:21
|
作者
Mukherjee, Dwaipayan [1 ]
Kumar, Shashi Ranjan [1 ]
机构
[1] Indian Inst Technol, Mumbai 400076, Maharashtra, India
关键词
Acceleration; Lyapunov methods; Time factors; Navigation; Switches; Lead; Kinematics; Barrier Lyapunov function; deviated pursuit; field-of-view (FOV); guidance; impact time; SLIDING-MODE CONTROL; SALVO ATTACK; LAW DESIGN; INTERCEPTION; CONSENSUS; MISSILES; SEEKER;
D O I
10.1109/TAES.2021.3074202
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article proposes a guidance strategy that enables the interceptor to control its impact time against stationary targets, while also meeting the field-of-view (FOV) constraints of the on-board seeker. The guidance strategy, so designed, always keeps the target within its FOV using its seeker. A barrier Lyapunov function is used to meet the FOV constraints, and an approximate expression for the interceptor's lead angle is obtained analytically. This facilitates the computation, as well as control, of impact time. The proposed guidance consists of two stages, with the former stage being deviated pursuit, while during the latter stage, the deviation angle or lead angle decreases to zero. This, in turn, ensures a zero terminal lateral acceleration. Furthermore, through a cooperative selection of tuning parameters, simultaneous interception of the target by multiple interceptors (also called salvo) can be achieved. Simulations, that are run for different engagement scenarios and with varying tuning parameters, vindicate the efficacy of the proposed strategy.
引用
收藏
页码:3296 / 3306
页数:11
相关论文
共 50 条
  • [11] Analytical solution of field-of-view limited guidance with constrained impact and capturability analysis
    Han, Tuo
    Hu, Qinglei
    Xin, Ming
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 97
  • [12] Impact Time and Angle Control Optimal Guidance with Field-of-View Constraint
    Chen, Ye
    Wu, Shufan
    Wang, Xiaoliang
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2022, 45 (12) : 2369 - 2378
  • [13] Polynomial Shaping-based Field -of-View Constrained Impact Time Guidance against Non-maneuvering Targets
    Surve, Prajakta
    Maity, Arnab
    Kumar, Shashi Ranjan
    IFAC PAPERSONLINE, 2022, 55 (22): : 406 - 411
  • [14] Three-Dimensional Nonsingular Impact Time Guidance With Limited Field-of-View
    Kumar, Shashi Ranjan
    Mukherjee, Dwaipayan
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2022, 30 (04) : 1448 - 1459
  • [15] Impact Time Control Guidance Considering Seeker's Field-of-View Limits
    Kim, Hyeong-Geun
    Kim, H. Jin
    2016 IEEE 55TH CONFERENCE ON DECISION AND CONTROL (CDC), 2016, : 4160 - 4165
  • [16] Field-of-View Limited Guidance with Constrained Impact via Line-of-Sight Shaping Approach
    Xi, Yong
    Han, Tuo
    Hu, Qinglei
    Zhong, Kewei
    PROCEEDINGS OF THE 2019 31ST CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2019), 2019, : 2974 - 2978
  • [17] Polynomial shaping based three-dimensional impact angle and field-of-view constrained guidance
    Surve, Prajakta
    Maity, Arnab
    Kumar, Shashi Ranjan
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 147
  • [18] Fixed Final Time Field of View and Impact Angle Constrained Guidance
    Ramesh, D.
    Maity, Arnab
    Sarkar, A. K.
    Umakant, J.
    2019 27TH MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION (MED), 2019, : 124 - 129
  • [19] Nonsingular Sliding Mode Guidance Law for Impact Time Control With Field-of-View Constraint
    Zhang, Lei
    Yi, Wenjun
    Guan, Jun
    IEEE ACCESS, 2025, 13 : 32004 - 32015
  • [20] Impact Angle and Time Control Guidance Under Field-of-View Constraints and Maneuver Limits
    Sang-Wook Shim
    Seong-Min Hong
    Gun-Hee Moon
    Min-Jea Tahk
    International Journal of Aeronautical and Space Sciences, 2018, 19 : 217 - 226