All Mechanical Primary Flight Control System for VTOL/STOL Aircraft

620481

01/01/1962

Authors Abstract
Content
This paper describes the development of a mechanism for the conversion of a human pilot's control stick or pedal displacement commands into differentiated output power commands or any desired sum or combination of the displacement command and successive differentiations. By this means the pilot's task of controlling a VTOL airplane during the VTOL phases of flight is reduced to where ordinary piloting technique is adequate.
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DOI
https://doi.org/10.4271/620481
Pages
8
Citation
Morris, W., "All Mechanical Primary Flight Control System for VTOL/STOL Aircraft," SAE Technical Paper 620481, 1962, https://doi.org/10.4271/620481.
Additional Details
Publisher
Published
Jan 1, 1962
Product Code
620481
Content Type
Technical Paper
Language
English