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NASA NTRS · 19740002188

Compensation based on linearized analysis for a six degree of freedom motion simulator

Abstract

The inertial response characteristics of a synergistic, six-degree-of-freedom motion base are presented in terms of amplitude ratio and phase lag as functions of frequency data for the frequency range of interest (0 to 2 Hz) in real time, digital, flight simulators. The notch filters which smooth the digital-drive signals to continuous drive signals are presented, and appropriate compensation, based on the inertial response data, is suggested. The existence of an inverse transformation that converts actuator extensions into inertial positions makes it possible to gather the response data in the inertial axis system.

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BibTeXRIS

Parrish, R. V., Dieudonne, J. E., Martin, D. J., Jr., Copeland, J. L.. 1973-11-01. Compensation based on linearized analysis for a six degree of freedom motion simulator. https://ntrs.nasa.gov/citations/19740002188

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