Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraint

Published 2013 View Full Article

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Title
Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraint
Authors
Keywords
-
Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 31, Issue 1, Pages 30-41
Publisher
Elsevier BV
Online
2013-09-19
DOI
10.1016/j.ast.2013.09.003

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