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Redundancy management of electrohydraulic servoactuators by mathematical model referencingA description of a mathematical model reference system is presented which provides redundancy management for an electrohydraulic servoactuator. The mathematical model includes a compensation network that calculates reference parameter perturbations induced by external disturbance forces. This is accomplished by using the measured pressure differential data taken from the physical system. This technique was experimentally verified by tests performed using the H-1 engine thrust vector control system for Saturn IB. The results of these tests are included in this report. It was concluded that this technique improves the tracking accuracy of the model reference system to the extent that redundancy management of electrohydraulic servosystems may be performed using this method.
Document ID
19720004489
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Campbell, R. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
November 9, 1971
Subject Category
Electronic Equipment
Report/Patent Number
NASA-TM-X-64625
Report Number: NASA-TM-X-64625
Accession Number
72N12138
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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