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Proceedings Paper

Improvements in the transient fidelity of HWIL flight tables using acceleration feedback
Author(s): Michael Swamp; Colin Stevens; Peter Hoffstetter
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Paper Abstract

Control system architecture will help eliminate or reduce non-linear behavior of flight table axes motions. This elimination and reduction will help improve dynamic transparency in HWIL simulations. This paper presents the design, analysis and test results of a three-axis hydraulic flight table using acceleration feedback as a part of the axes servo structure. This approach significantly improves the transient motion of the axis under control producing a very high fidelity flight motion table.

Paper Details

Date Published: 12 July 2002
PDF: 14 pages
Proc. SPIE 4717, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VII, (12 July 2002); doi: 10.1117/12.474725
Show Author Affiliations
Michael Swamp, Acutronic USA, Inc. (United States)
Colin Stevens, Acutronic Schweiz AG (Switzerland)
Peter Hoffstetter, Acutronic Schweiz AG (Switzerland)

Published in SPIE Proceedings Vol. 4717:
Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VII
Robert Lee Murrer Jr., Editor(s)

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