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Remote manipulator system flexibility analysis program: Mission planning, mission analysis, and software formulationA computer program is described for calculating the flexibility coefficients as arm design changes are made for the remote manipulator system. The coefficients obtained are required as input for a second program which reduces the number of payload deployment and retrieval system simulation runs required to simulate the various remote manipulator system maneuvers. The second program calculates end effector flexibility and joint flexibility terms for the torque model of each joint for any arbitrary configurations. The listing of both programs is included in the appendix.
Document ID
19790001945
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kumar, L.
(McDonnell-Douglas Astronautics Co. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
August 10, 1978
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-151830
PAPER-1.4-7-245
Report Number: NASA-CR-151830
Report Number: PAPER-1.4-7-245
Accession Number
79N10116
Funding Number(s)
CONTRACT_GRANT: NAS9-15550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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