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The use of the power spectral density function to measure the effects of motion on an aircraft simulation

Published online by Cambridge University Press:  04 July 2016

W. H. Ekin  and
D. McCloy
W. H. Ekin
Affiliation:
Robert Gordon's Institute of Technology, Aberdeen
D. McCloy
Affiliation:
The Ulster Polytechnic
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Extract

Although hundreds of moving base simulators exist in the world today, there is a paucity of objective and quantitative methods of assessing the necessity for, and the effectiveness of the motion provided. This paper describes a quantitative method of assessing the effects of motion on an aircraft simulation when there is short-term interactive control of the aircraft by the pilot.

Type
Research Article
Information
The Aeronautical Journal , Volume 84 , Issue 831 , April 1980 , pp. 101 - 107
Copyright
Copyright © Royal Aeronautical Society 1980 

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Footnotes

*

Lecturer, School of Mechanical and Offshore Engineering. Formerly Research Associate, Department of Aeronautical Engineering, Queen's University of Belfast.

†

Professor and Head of School of Industrial and Mechanical Engineering, the Ulster Polytechnic. Formerly Professor of Aeronautical Engineering, Queen's University of Belfast.

References

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4. Wilcox, T. A simulation of the low speed handling of the BAC 221 slender-wing research aircraft. R & M 3670, 1971.Google Scholar
5. Ekin, W. H. A quantitative investigation of the effects of motion on an aircraft simulation. PhD Thesis, QUB, 1977.Google Scholar