Suboptimal guidance law against maneuvering target with time and angle constraints

The impact time and angle constrained terminal guidance laws against a maneuvering target are usually designed under the assumption that the magnitude of the missile's velocity can be controlled, rather than a missile with uncontrollable speed because it is difficult to adjust the time-to-go du...

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Veröffentlicht in:	Aerospace science and technology Jg. 148; S. 109111
Hauptverfasser:	Xie, Jiliang, Ma, Kemao
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Masson SAS 01.05.2024
Schlagworte:	Impact time constraint Optimal guidance law Terminal angle constraint Terminal guidance Impact time constraint Optimal guidance law Terminal angle constraint Terminal guidance
ISSN:	1270-9638
Online-Zugang:	Volltext
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