Development of The Lockheed L-1011's Flying Stabilizer

710426

02/01/1971

Authors
Abstract
Content
Longitudinal control on the Lockheed L-1011 is provided by a flying stabilizer. This is the first time such an approach has been used on a United States commercial jet transport.
This paper presents the reasons for the choice of longitudinal control systems, and describes the mechanization of the control system with particular emphasis on how it meets Lockheed's safety standards and the Federal Airworthiness Requirements. The status of the ground and flight development tests is discussed.
Meta TagsDetails
DOI
https://doi.org/10.4271/710426
Pages
14
Citation
Whitmore, C., "Development of The Lockheed L-1011's Flying Stabilizer," SAE Technical Paper 710426, 1971, https://doi.org/10.4271/710426.
Additional Details
Publisher
Published
Feb 1, 1971
Product Code
710426
Content Type
Technical Paper
Language
English