Equations for intermediate range missile, presented in form suitable for application of differential analyzer and digital computer techniques, provide description of mo tion of aerodynamically controlled winged vehicles and are applicable to terminal accuracy and dynamic stability studies where higher order effects are of interest.
General air-frame dynamics of guided missile
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 8
1955
7 pages
Article (Journal)
English
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