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Optimal control/structure integrated design of a flexible space platform with articulated appendagesA complete set of closed form symbolic equations are developed for a 2-D model of a system comprised of a flexible platform with articulated appendages. The system considered has a flexible two link manipulator, with joint compliance, at one end of the flexible platform and an articulated antenna on the other end. The model is formulated using a Lagrangian approach which incorporates homogeneous transformation matrices, similar to those typically seen in the robotics literature, for the kinematic representation. The integrated control/structure design strategy considered emphasizes rapid system response and minimal structural weight. Constraints are included to keep antenna pointing error to a minimum, and at the same time achieve accurate end point positioning of the manipulator with minimal oscillations.
Document ID
19930038025
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kelkar, Atul G.
(NASA Langley Research Center Hampton, VA, United States)
Alberts, Thomas E.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Structures sensing and control; Proceedings of the Meeting, Orlando, FL, Apr. 2, 3, 1991 (A93-22001 07-35)
Publisher: Society of Photo-Optical Instrumentation Engineers
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93A22022
Funding Number(s)
CONTRACT_GRANT: NAS1-185481
Distribution Limits
Public
Copyright
Other

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