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Variable feel simulation

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 August 1972

22

Abstract

VARIABLE FEEL SYSTEMS were developed to provide the pilots of high‐performance jet aircraft — equipped with powered flying controls — with simulated aerodynamic reaction forces at the controls. These systems provide the primary factor in determining the handling characteristics of the aircraft, and replace the “Natural feel” forces previously available in low‐speed aircraft, through the direct natural aerodynamic reaction at the controls.

Citation

(1972), "Variable feel simulation", Aircraft Engineering and Aerospace Technology, Vol. 44 No. 8, pp. 8-11. https://doi.org/10.1108/eb034929

Publisher

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MCB UP Ltd

Copyright © 1972, MCB UP Limited

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