Three-dimensional cooperative guidance laws with impact velocity and impact angles constraints

In this paper, we propose a cooperative guidance algorithm designed to enable multiple missiles to simultaneously attack a target at desired terminal angles while maintaining control over their impact velocities. The three-dimensional (3-D) guidance laws incorporate a guidance law along the line-of-...

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Veröffentlicht in:	Aerospace science and technology Jg. 159; S. 109997
Hauptverfasser:	Li, Yajun, Zhu, Mingjia, An, Binghe, Zhi, Yongran, Liu, Lei, Fan, Huijin, Wang, Bo
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Masson SAS 01.04.2025
Schlagworte:	Cooperative guidance algorithm Fixed-time control Impact angle Impact velocity Impact velocity Fixed-time control Cooperative guidance algorithm Impact angle
ISSN:	1270-9638
Online-Zugang:	Volltext
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