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A Fluidically-Augmented Artificial Feel System for High Performance Aircraft
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1970 by SAE International in United States
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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.
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CitationJansen, 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.
- “The Artificial Feel System,” BuAer Report. AE-61-4 V May 1953
- Kutz G. Fortenbaug R. “A Method for Bobweight Feel System Design.” Grumman Aircraft Engr. Corp. Rept. No. 394-68-2 Jan. 17 1969
- Sipa Nicholas J. “Characteristics of Longitudinal Control Feel Systems Used in Fighter Aircraft.” Bureau of Aeronautics TED Project ADC AE-6101 Nov. 5 1959
- Kaniuka Walter W. “Development of a Fluidic Angular Acceleration Sensor.” Naval Air Development Center Report No. NADC-AM-6919 May 2 1969
- Kaniuka Walter W. Sweeney James C. “An Investigation of the Feasibility of Using Fluidic Devices to Improve the Performance of Artificial Feel Systems.” Interim Report, Naval Air Development Center Report No. NADC-AM-7016 April 28 1970