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Design, characterization and control of the Unique Mobility Corporation robotSpace and mass are at a premium on any space mission, and thus any machinery designed for space use should be lightweight and compact, without sacrificing strength. It is for this reason that NASA/LeRC contracted Unique Mobility Corporation to exploit their novel actuator designs to build a robot that would advance the present state of technology with respect to these requirements. Custom-designed motors are the key feature of this robot. They are compact, high-performance dc brushless servo motors with a high pole count and low inductance, thus permitting high torque generation and rapid phase commutation. Using a custom-designed digital signal processor-based controller board, the pulse width modulation power amplifiers regulate the fast dynamics of the motor currents. In addition, the programmable digital signal processor (DSP) controller permits implementation of nonlinear compensation algorithms to account for motoring vs. regeneration, torque ripple, and back-EMF. As a result, the motors produce a high torque relative to their size and weight, and can do so with good torque regulation and acceptably high velocity saturation limits. This paper presents the Unique Mobility Corporation robot prototype: its actuators, its kinematic design, its control system, and its experimental characterization. Performance results, including saturation torques, saturation velocities and tracking accuracy tests are included.
Document ID
19940028790
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Velasco, Virgilio B., Jr.
(Case Western Reserve Univ. Cleveland, OH., United States)
Newman, Wyatt S.
(Case Western Reserve Univ. Cleveland, OH., United States)
Steinetz, Bruce
(NASA Lewis Research Center Cleveland, OH, United States)
Kopf, Carlo
(NASA Lewis Research Center Cleveland, OH, United States)
Malik, John
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Publication Information
Publication: The 28th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
94N33296
Funding Number(s)
CONTRACT_GRANT: NAS3-26285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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