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Servomotor and Controller Having Large Dynamic RangeA recently developed micro-commanding rotational-position-control system offers advantages of less mechanical complexity, less susceptibility to mechanical resonances, less power demand, less bulk, less weight, and lower cost, relative to prior rotational-position-control systems based on stepping motors and gear drives. This system includes a digital-signal- processor (DSP)-based electronic controller, plus a shaft-angle resolver and a servomotor mounted on the same shaft. Heretofore, micro-stepping has usually been associated with stepping motors, but in this system, the servomotor is micro-commanded in response to rotational-position feedback from the shaft-angle resolver. The shaft-angle resolver is of a four-speed type chosen because it affords four times the resolution of a single-speed resolver. A key innovative aspect of this system is its position-feedback signal- conditioning circuits, which condition the resolver output signal for multiple ranges of rotational speed. In the preferred version of the system, two rotational- speed ranges are included, but any number of ranges could be added to expand the speed range or increase resolution in particular ranges. In the preferred version, the resolver output is conditioned with two resolver-to-digital converters (RDCs). One RDC is used for speeds from 0.00012 to 2.5 rpm; the other RDC is used for speeds of 2.5 to 6,000 rpm. For the lower speed range, the number of discrete steps of RDC output per revolution was set at 262,144 (4 quadrants at 16 bits per quadrant). For the higher speed range, the number of discrete steps per revolution was set at 4,096 (4 quadrants at 10 bits per quadrant).
Document ID
20090041680
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Alhorn, Dean C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Howard, David E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Smith, Dennis A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Dutton, Ken
(Madison Research Corp. Huntsville, AL, United States)
Paulson, M. Scott
(Mevatec Corp. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2007
Publication Information
Publication: NASA Tech Briefs, March 2007
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-31529-1
Distribution Limits
Public
Copyright
Public Use Permitted.
Patent
US-Patent-7,081,730
Patent Application
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