Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane

Brown, B. Porter., Chilton, Robert G., Whitten, James B.
naca-report-1101
1952


Report presents the results of measurements of the longitudinal stability and control characteristics of a large airplane using a mechanical feel device in combination with a booster incorporated in the elevator-control system. Tests were made to investigate the feasibility of eliminating the aerodynamic control forces through use of a booster and of providing control-feel forces mechanically. The feel device consisted of a centering spring which restrained the control stick through a linkage which was changed as a function of the dynamic pressure. Provisions were made for trimming and for manual adjustment of the force gradient. The system was designed to approximate the control-force characteristics that would result with a conventional elevator control with linear hinge-moment characteristics.

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http://naca.central.cranfield.ac.uk/reports/1952/naca-report-1101.pdf