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Resonance-inert stabilization for space stationsAn approach to stabilizing control systems is presented which structures controllers like passive mechanical systems. The controller is visualized as a structural part with a passive behavior similar to springs, dashpots, and masses. If such a controller is connected by a proper feedback arrangement, then a passive mechanical plant cannot upset stability, regardless of masses, resonances, and three-dimensional coupling. The concept of resonance-inert stabilization is explained by structuring the controller of a simple feedback loop. Reactive functions, connections, and matrices are defined and used in the stabilization concept. The realization of a possible Skylab control system is discussed and compared with the present design. This example demonstrates the applicability to three-dimensional problems with lagging controllers.
Document ID
19720017627
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Vonpragenau, G. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1972
Subject Category
Electronics
Report/Patent Number
M-214
NASA-TN-D-6731
Report Number: M-214
Report Number: NASA-TN-D-6731
Accession Number
72N25277
Funding Number(s)
PROJECT: RTOP 908-10-08-0000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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