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Mechanism test bed. Flexible body model reportThe Space Station Mechanism Test Bed is a six degree-of-freedom motion simulation facility used to evaluate docking and berthing hardware mechanisms. A generalized rigid body math model was developed which allowed the computation of vehicle relative motion in six DOF due to forces and moments from mechanism contact, attitude control systems, and gravity. No vehicle size limitations were imposed in the model. The equations of motion were based on Hill's equations for translational motion with respect to a nominal circular earth orbit and Newton-Euler equations for rotational motion. This rigid body model and supporting software were being refined.
Document ID
19910020847
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Compton, Jimmy
(Control Dynamics Co. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-184189
NAS 1.26:184189
Report Number: NASA-CR-184189
Report Number: NAS 1.26:184189
Accession Number
91N30161
Funding Number(s)
CONTRACT_GRANT: NAS8-38771
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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