Predefined-Time Spatial-Temporal Cooperative Guidance Law With Leader-Follower Strategy

In this article, a 3-D cooperative guidance law using a leader-follower strategy is proposed for a multimissile simultaneous attack on a maneuvering target at an adjustable impact time and desired impact angles. Since the missile terminal guidance phase spans a very short time, predefined-time conve...

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Vydané v:	IEEE transactions on aerospace and electronic systems Ročník 61; číslo 3; s. 6053 - 6069
Hlavní autori:	Wang, Xu, Cai, Yuanli, Deng, Yifan, Jiang, Haonan
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New York IEEE 01.06.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Predmet:	adaptive control Aerospace and electronic systems asymptotic stability Communication networks Consensus protocol Control methods Control theory Convergence Design Design parameters Disturbance observers Initial conditions Line of sight Lyapunov methods Maneuvering targets Missile control Missile tracking Missiles multi-agent systems Navigation numerical simulation Simulation Sliding mode control Stability analysis State observers Terminal guidance Topology Upper bound
ISSN:	0018-9251, 1557-9603
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