A Fluidically-Augmented Artificial Feel System for High Performance Aircraft 700785
Of the several types of pitch axis artificial feel systems currently in use in fighter and attack aircraft the most common is the bobweight, spring, and viscous damper type, and variations on it. The current project of NAVAIRDEVCEN is to augment and improve this type of feel system through the use of fluidic devises. Such augmentation will improve the handling qualities of aircraft by reducing variations in stick force for a given maneuvering response; will reduce the weight and inertia of the feel system; will permit tailoring of the feel system performance over the flight envelope.
Citation: Jansen, T. and Kaniuka, W., "A Fluidically-Augmented Artificial Feel System for High Performance Aircraft," SAE Technical Paper 700785, 1970, https://doi.org/10.4271/700785. Download Citation
Author(s):
Tor W. Jansen, Walter W. Kaniuka
Affiliated:
Aero Mechanics Dept., Naval Air Development Center
Pages: 16
Event:
National Aeronautic and Space Engineering and Manufacturing Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Aircraft
Springs
Pitch
Dampers and shock absorbers
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