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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Vydané v:	Aerospace science and technology Ročník 148; s. 109111
Hlavní autori:	Xie, Jiliang, Ma, Kemao
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Elsevier Masson SAS 01.05.2024
Predmet:	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
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