航向(导航)
比例导航
拦截
控制理论(社会学)
计算机科学
归巢(生物学)
理论(学习稳定性)
李雅普诺夫函数
工程类
人工智能
控制(管理)
导弹
航空航天工程
物理
非线性系统
机器学习
生物
量子力学
生态学
作者
Shashi Ranjan Kumar,Dwaipayan Mukherjee
标识
DOI:10.1016/j.ast.2022.107499
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.
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