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Design and Development of the Fail Operative Automatic Landing System for the Lockheed L-1011

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Gorham, John A., author.
Conference Name:
National Air Transportation Meeting (1969-04-21 : New York, New York, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1969
Summary:
This paper describes the operational characteristics, design processes, and test programs established to produce a "fail-operative" automatic landing system for the Lockheed "TriStar." The operational characteristics are predicated on the anticipated changes in ATC procedures during the 1970's which may lead to increased automation of the airborne elements. The design processes involve the use of new electronic voting techniques and the consideration of the total airplane systems in view of the critical aspects of failure modes and effects. The test program is outlined and the use of many iterative stages of comprehensive test facilities are described. Conclusions are made that unexpected benefits have been derived by the adoption of the total systems approach
Notes:
Vendor supplied data
Publisher Number:
690407
Access Restriction:
Restricted for use by site license

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