Algebraic functions for each plane of motion, roll, pitch, and yaw, of airframe derived, assuming there is no cross coupling between planes; by use of suitable parameters they have been put in standard servomechanism form, thus assisting design and analysis of control systems for airframes.
Derivation and use of aerodynamic transfer functions of airframes
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 59 , n 539
1955
19 pages
Article (Journal)
English
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