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Applications of Fluidics to Light Aircraft Instrumentation and Control

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Garner, H. D., author.
Conference Name:
National Business Aircraft Meeting and Engineering Display (1974-04-02 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1974
Summary:
This paper reviews NASA/Langley's program for the development of advanced fluidic components and the application of these components to general aviation instrumentation and control. The major project in this category has been the development of a simple, reliable, two-axis autopilot for light aircraft, using a fluidic inertial rate sensor for stability and roll attitude control, and a simple magnetometer for azimuth reference. This autopilot has been successfully flight tested. Fluidic hardware developed for this autopilot is described, and projected improvements and extensions are discussed. Application of fluidic components to such flight instruments as turn coordinators, artificial horizons, and true airspeed indicators is explored
Notes:
Vendor supplied data
Publisher Number:
740351
Access Restriction:
Restricted for use by site license

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