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Operational viewpoint of the X-29A digital flight control systemIn the past few years many flight control systems have been implemented as full-authority, full-time digital systems. The digital design has allowed flight control systems to make use of many enhanced elements that are generally considered too complex to implement in an analog system. Examples of these elements are redundant information exchanged between channels to allow for continued operation after multiple failures and multiple variable gain schedules to optimize control of the aircraft throughout its flight envelope and in all flight modes. The introduction of the digital system for flight control also created the problem of obtaining information from the system in an understandable and useful format. This paper presents how the X-29A was dealt with during its operations at NASA Ames-Dryden Flight Research Facility. A brief description of the X-29A control system, a discussion of the tools developed to aid in daily operations, and the troubleshooting of the aircraft are included.
Document ID
19880011768
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chacon, Vince
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Mcbride, David
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:100434
H-1467
NASA-TM-100434
Report Number: NAS 1.15:100434
Report Number: H-1467
Report Number: NASA-TM-100434
Accession Number
88N21152
Funding Number(s)
PROJECT: RTOP 533-05-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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