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Primary reaction control system/remote manipulator system interaction with loaded arm. Space shuttle engineering and operations supportA study of the interaction between the orbiter primary reaction control system (PRCS) and the remote manipulator system (RMS) with a loaded arm is documented. This analysis was performed with the Payload Deployment and Retrieval Systems Simulation (PDRSS) program with the passive arm bending option. The passive-arm model simulates the arm as massless elastic links with locked joints. The study was divided into two parts. The first part was the evaluation of the response of the arm to step inputs (i.e. constant jet torques) about each of the orbiter body axes. The second part of the study was the evaluation of the response of the arm to minimum impulse primary RCS jet firings with both single pulse and pulse train inputs.
Document ID
19780016329
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Taylor, E. C.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Davis, J. D.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
May 23, 1978
Subject Category
Space Transportation
Report/Patent Number
WORKING-PAPER-1.4-7-229
NASA-CR-151721
Report Number: WORKING-PAPER-1.4-7-229
Report Number: NASA-CR-151721
Accession Number
78N24272
Funding Number(s)
CONTRACT_GRANT: NAS9-15550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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