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NASA/MSFC ground experiment for large space structure control verificationMarshall Space Flight Center has developed a facility in which closed loop control of Large Space Structures (LSS) can be demonstrated and verified. The main objective of the facility is to verify LSS control system techniques so that on orbit performance can be ensured. The facility consists of an LSS test article which is connected to a payload mounting system that provides control torque commands. It is attached to a base excitation system which will simulate disturbances most likely to occur for Orbiter and DOD payloads. A control computer will contain the calibration software, the reference system, the alignment procedures, the telemetry software, and the control algorithms. The total system will be suspended in such a fashion that LSS test article has the characteristics common to all LSS.
Document ID
19850012938
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Waites, H. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Seltzer, S. M.
(Control Dyamics Co.)
Tollison, D. K.
(Control Dynamics Co.)
Date Acquired
September 5, 2013
Publication Date
December 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:86496
NASA-TM-86496
Report Number: NAS 1.15:86496
Report Number: NASA-TM-86496
Accession Number
85N21248
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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