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A Unique Approach to the Development of a Light Helicopter Automatic Flight Control System

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Korte, Donald R., 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:
The requirements and implementation of the Enstrom Cruise-A-Long flight control system are described. This includes a review of the need for better helicopter stability, in terms of pilot work load, and separation of maneuverability from stability.The flight control system configuration is defined with block diagrams, hardware implementation, actuation analysis, and failure monitoring. System interface with aircraft performance characteristics, along with flight test results, are highlighted
Notes:
Vendor supplied data
Publisher Number:
740348
Access Restriction:
Restricted for use by site license

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