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LQC control for the Mini-Mast experimentThe Mini-Mast system is briefly reviewed, and results of a simulation study of the LQG control for the Mini-Mast experiment are reported. In particular, attention is given to problems and limitations related to the testing of control laws using reaction mass actuators, such as accounting for force and stroke limits of these devices. The local controller used in the study and the algorithm for converting the force commands of the LQG algorithm to position commands for the reaction mass device are described. It is shown that the LQG generated damping is reduced when a local controller is used and the position command is not saturated; it drops still further when the position command is saturated.
Document ID
19890024320
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Montgomery, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Ghosh, D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: VPI&SU/AIAA Symposium
Location: Blacksburg, VA
Country: United States
Start Date: June 29, 1987
End Date: July 1, 1987
Accession Number
89A11691
Distribution Limits
Public
Copyright
Other

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