True-proportional-navigation inspired finite-time homing guidance for time constrained interception

被引:16
作者
Kumar, Shashi Ranjan [1 ]
Mukherjee, Dwaipayan [2 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Intelligent Syst & Control Lab, Mumbai 400076, Maharashtra, India
[2] Indian Inst Technol, Dept Elect Engn, Mumbai 400076, Maharashtra, India
关键词
True proportional navigation; Impact time guidance; Homing guidance; Maneuvering target; Lyapunov stability theory; Finite time convergence; IMPACT-TIME; COOPERATIVE GUIDANCE; SIMULTANEOUS ATTACK; MULTIPLE MISSILES; LAW; TARGET; ANGLE; DESIGN;
D O I
10.1016/j.ast.2022.107499
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper addresses the problem of controlling impact time against various types of target - stationary, constant velocity, or maneuvering. Analytical expression of time-to-go, that is exact for non-maneuvering target but approximate for maneuvering ones, is first presented based on true-proportional-navigation guidance concepts. Guidance strategies are then derived, using Lyapunov theory, to meet impact time constraints, without linearizing the engagement dynamics. Hence, the proposed strategies remain effective even for large initial heading errors. Further, a cooperative guidance strategy to achieve simultaneous target interception by multiple interceptors is also proposed. Guidance commands that ensure consensus among the time-to-go values of the interceptors are utilized for this purpose. Using judicious choices of gains, the common time of target interception may be either pre-fixed, or the same may be decided cooperatively during the engagement. Stability analysis of the possible equilibria in heading angle dynamics, for different choices of parameters, is also performed. For both one-to-one and cooperative homing, simulation results are presented for various engagement scenarios to demonstrate the effectiveness of the proposed strategies. (C) 2022 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:19
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