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A Comprehensive C++ Controller for a Magnetically Supported Vertical RotorThis manual describes the new FATMaCC (Five-Axis, Three-Magnetic-Bearing Control Code). The FATMaCC (pronounced "fat mak") is a versatile control code that possesses many desirable features that were not available in previous in-house controllers. The ultimate goal in designing this code was to achieve full rotor levitation and control at a loop time of 50 microsec. Using a 1-GHz processor, the code will control a five-axis system in either a decentralized or a more elegant centralized (modal control) mode at a loop time of 56 microsec. In addition, it will levitate and control (with only minor modification to the input/output wiring) a two-axis and/or a four-axis system. Stable rotor levitation and control of any of the systems mentioned above are accomplished through appropriate key presses to modify parameters, such as stiffness, damping, and bias. A signal generation block provides 11 excitation signals. An excitation signal is then superimposed on the radial bearing x- and y-control signals, thus producing a resultant force vector. By modulating the signals on the bearing x- and y-axes with a cosine and a sine function, respectively, a radial excitation force vector is made to rotate 360 deg. about the bearing geometric center. The rotation of the force vector is achieved manually by using key press or automatically by engaging the "one-per-revolution" feature. Rotor rigid body modes can be excited by using the excitation module. Depending on the polarities of the excitation signal in each radial bearing, the bounce or tilt mode will be excited.
Document ID
20010047391
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Morrison, Carlos R.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2001
Subject Category
Engineering (General)
Report/Patent Number
NAS 1.15:210701
E-12632
NASA/TM-2001-210701
Report Number: NAS 1.15:210701
Report Number: E-12632
Report Number: NASA/TM-2001-210701
Funding Number(s)
PROJECT: RTOP 708-28-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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