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                                       Details for article 11 of 12 found articles
 
 
  Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraint
 
 
Title: Terminal guidance laws of missile based on ISMC and NDOB with impact angle constraint
Author: Zhang, Zhenxing
Li, Shihua
Luo, Sheng
Appeared in: Aerospace science and technology
Paging: Volume 31 (2013) nr. 1 pages 12 p.
Year: 2013
Contents:
Publisher: Elsevier Masson SAS
Source file: Elektronische Wetenschappelijke Tijdschriften
 
 

                             Details for article 11 of 12 found articles
 
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