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Experience with synchronous and asynchronous digital control systemsFlight control systems have undergone a revolution since the days of simple mechanical linkages; presently the most advanced systems are full-authority, full-time digital systems controlling unstable aircraft. With the use of advanced control systems, the aerodynamic design can incorporate features that allow greater performance and fuel savings, as can be seen on the new Airbus design and advanced tactical fighter concepts. These advanced aircraft will be and are relying on the flight control system to provide the stability and handling qualities required for safe flight and to allow the pilot to control the aircraft. Various design philosophies have been proposed and followed to investigate system architectures for these advanced flight control systems. One major area of discussion is whether a multichannel digital control system should be synchronous or asynchronous. This paper addressed the flight experience at the Dryden Flight Research Facility of NASA's Ames Research Center with both synchronous and asynchronous digital flight control systems. Four different flight control systems are evaluated against criteria such as software reliability, cost increases, and schedule delays.
Document ID
19860020394
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Regenie, V. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Chacon, C. V.
(NASA Ames Research Center Moffett Field, CA, United States)
Lock, W. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 86-2239-CP
H-1372
NAS 1.15:88271
NASA-TM-88271
Report Number: AIAA PAPER 86-2239-CP
Report Number: H-1372
Report Number: NAS 1.15:88271
Report Number: NASA-TM-88271
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Williamsburg, VA
Country: United States
Start Date: August 18, 1986
End Date: August 20, 1986
Accession Number
86N29866
Funding Number(s)
PROJECT: RTOP 505-66-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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