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Distributed control using linear momentum exchange devicesMSFC has successfully employed the use of the Vibrational Control of Space Structures (VCOSS) Linear Momentum Exchange Devices (LMEDs), which was an outgrowth of the Air Force Wright Aeronautical Laboratory (AFWAL) program, in a distributed control experiment. The control experiment was conducted in MSFC's Ground Facility for Large Space Structures Control Verification (GF/LSSCV). The GF/LSSCV's test article was well suited for this experiment in that the LMED could be judiciously placed on the ASTROMAST. The LMED placements were such that vibrational mode information could be extracted from the accelerometers on the LMED. The LMED accelerometer information was processed by the control algorithms so that the LMED masses could be accelerated to produce forces which would dampen the vibrational modes of interest. Experimental results are presented showing the LMED's capabilities.
Document ID
19870015088
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sharkey, J. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Waites, Henry
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Doane, G. B., III
(Control Dynamics Co. Huntsville, Ala., United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:100308
NASA-TM-100308
Report Number: NAS 1.15:100308
Report Number: NASA-TM-100308
Accession Number
87N24521
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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