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Development and simulations of aircraft guidance system using a 3–degree‐of‐freedom point mass model

✍ Scribed by Sudars, Martins

Book ID: 126607617
Publisher: Vilnius Gediminas Technical University
Year: 2009
Tongue: English
Weight: 648 KB
Volume: 13
Category: Article
ISSN: 1648-7788
DOI: 10.3846/1648-7788.2009.13.35-43

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