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A compact roller-gear pitch-yaw joint module: Design and control issuesRobotic systems have been proposed as a means of accomplishing assembly and maintenance tasks in space. The desirable characteristics of these systems include compact size, low mass, high load capacity, and programmable compliance to improve assembly performance. In addition, the mechanical system must transmit power in such a way as to allow high performance control of the system. Efficiency, linearity, low backlash, low torque ripple, and low friction are all desirable characteristics. This work presents a pitch-yaw joint module designed and built to address these issues. Its effectiveness as a two degree-of-freedom manipulator using natural admittance control, a method of force control, is demonstrated.
Document ID
19940025126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dohring, Mark E.
(Case Western Reserve Univ. Cleveland, OH., United States)
Anderson, William J.
(NASTEC, Inc. Cleveland, OH., United States)
Newman, Wyatt S.
(Case Western Reserve Univ. Cleveland, OH., United States)
Rohn, Douglas A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Publication Information
Publication: NASA. Ames Research Center, The 27th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
94N29629
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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