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An actuator extension transformation for a motion simulator and an inverse transformation applying Newton-Raphson's methodA set of equations which transform position and angular orientation of the centroid of the payload platform of a six-degree-of-freedom motion simulator into extensions of the simulator's actuators has been derived and is based on a geometrical representation of the system. An iterative scheme, Newton-Raphson's method, has been successfully used in a real time environment in the calculation of the position and angular orientation of the centroid of the payload platform when the magnitude of the actuator extensions is known. Sufficient accuracy is obtained by using only one Newton-Raphson iteration per integration step of the real time environment.
Document ID
19730003455
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dieudonne, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Computers
Report/Patent Number
NASA-TN-D-7067
L-8505
Report Number: NASA-TN-D-7067
Report Number: L-8505
Accession Number
73N12182
Funding Number(s)
PROJECT: RTOP 501-39-11-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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