An actuator extension transformation for a motion simulator and an inverse transformation applying Newton-Raphson's method

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086 0 ‡aNAS 1.14:D-7067
088 ‡aNASA-TN-D-7067
100 1 ‡aDieudonne, James E.
245 1 3 ‡aAn actuator extension transformation for a motion simulator and an inverse transformation applying Newton-Raphson's method ‡h[electronic resource] / ‡cby James E. Dieudonne, Russell V. Parrish, and Richard E. Bardusch.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c[1972]
300 ‡a20 p.: ‡bill. ; ‡c26 cm.
490 0 ‡aNASA technical note; ‡vD-7067
500 ‡a"November 1972."--Cover.
500 ‡aMajor NASA subject terms: Motion, Newton-Raphson Method, Real Time Operation, Simulators, Actuators, Iteration, Numberical Analysis, Positioning.
500 ‡aPrepared at Langley Research Center.
504 ‡aIncludes bibliographical references p. 12.
520 ‡aA 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.
538 ‡aMode of access: Internet.
538 ‡aSystem requirements: Adobe Acrobat Reader.
538 ‡aMode of access: World Wide Web.
650 0 ‡aReal-time control.
650 0 ‡aTransformations (Mathematics)
650 0 ‡aIterative methods (Mathematics)
650 0 ‡aActuators.
650 0 ‡aFlight simulators ‡xAutomatic control.
700 1 ‡aBardusch, Richard E.
700 1 ‡aParrish, Russell V.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
710 2 ‡aLangley Research Center.
CID ‡a011449493
DAT 0 ‡a20101111091951.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-12-12T18:45:18Z
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