NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Modeling and simulation of a Stewart platform type parallel structure robotThe kinematics and dynamics of a Stewart Platform type parallel structure robot (NASA's Dynamic Docking Test System) were modeled using the method of kinematic influence coefficients (KIC) and isomorphic transformations of system dependence from one set of generalized coordinates to another. By specifying the end-effector (platform) time trajectory, the required generalized input forces which would theoretically yield the desired motion were determined. It was found that the relationship between the platform motion and the actuators motion was nonlinear. In addition, the contribution to the total generalized forces, required at the actuators, from the acceleration related terms were found to be more significant than the velocity related terms. Hence, the curve representing the total required actuator force generally resembled the curve for the acceleration related force. Another observation revealed that the acceleration related effective inertia matrix I sub dd had the tendency to decouple, with the elements on the main diagonal of I sub dd being larger than the off-diagonal elements, while the velocity related inertia power array P sub ddd did not show such tendency. This tendency results in the acceleration related force curve of a given actuator resembling the acceleration profile of that particular actuator. Furthermore, it was indicated that the effective inertia matrix for the legs is more decoupled than that for the platform. These observations provide essential information for further research to develop an effective control strategy for real-time control of the Dynamic Docking Test System.
Document ID
19890014504
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lim, Gee Kwang
(Texas Univ. Austin, TX, United States)
Freeman, Robert A.
(Texas Univ. Austin, TX, United States)
Tesar, Delbert
(Texas Univ. Austin, TX, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1989
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-184969
NAS 1.26:184969
Report Number: NASA-CR-184969
Report Number: NAS 1.26:184969
Accession Number
89N23875
Funding Number(s)
CONTRACT_GRANT: NAG9-188
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available