Investigations are made of effect of stiffness on stick travel per airplane response in steady longitudinal maneuvers, and on frequency response characteristics of airplane to stick movement during unaccelerated flight; calculations, including analog computer analysis of effect of stiffness on aircraft response in initial or transient state of longitudinal control, are made based on data of prototype airplane; development of concept and flight tests are described.
Research on improvement of flying qualities of piloted air-planes -- Reduced stiffness concept applied to elevator control system
Tokyo. Univ -- Inst Space Aeronautical Science -- Report
1965
80 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Flying qualities of a remotely piloted vehicle
AIAA | 1992
|Improvements in Flying Qualities of Modern Light Planes
SAE Technical Papers | 1963
|