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A brief analysis and its experiment of the hydraulic-electric loading servosystemThe servosystem is a force simulator. It can be used to simulate the hinge moment of the control surface for aircraft, and still be a stick force generator. According to the experiences of a real system, theoretical analyses of the loading system and its characteristics were performed and the possibility of improving its performances is discussed.
Document ID
19810010606
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Liango-Fu, M.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
HK-80071
NASA-TM-76458
Report Number: HK-80071
Report Number: NASA-TM-76458
Accession Number
81N19132
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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