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Proceedings Paper

Flight table orientation error transparency for hardware-in-the-loop facilities
Author(s): Nikos Andrianos; Christian Diez; Louis A. DeMore
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Paper Abstract

This paper presents the construction of the overall orientation error model based on the measurable table errors of axis wobble, axes non-orthogonality, axes intersection and axis encoding. With this model, the HWIL simulation engineer may, in the future, be able to calibrate and/or set requirements for the missile and target five-axis motion simulator to reduce the effect of the static orientation error on the simulation.

Paper Details

Date Published: 31 August 2001
PDF: 14 pages
Proc. SPIE 4366, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VI, (31 August 2001); doi: 10.1117/12.438076
Show Author Affiliations
Nikos Andrianos, Acutronic USA, Inc. (United States)
Christian Diez, DaimlerChrysler Aerospace (Germany)
Louis A. DeMore, Acutronic USA, Inc. (United States)

Published in SPIE Proceedings Vol. 4366:
Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VI
Robert Lee Murrer, Editor(s)

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