Flight table orientation error transparency for hardware-in-the-loop facilities

Nikos Andrianos; Christian Diez; Louis A. DeMore

doi:10.1117/12.438076

31 August 2001 Flight table orientation error transparency for hardware-in-the-loop facilities

Nikos Andrianos, Christian Diez, Louis A. DeMore

Proceedings Volume 4366, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VI; (2001) https://doi.org/10.1117/12.438076
Event: Aerospace/Defense Sensing, Simulation, and Controls, 2001, Orlando, FL, United States

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.

Citation Download Citation

Nikos Andrianos, Christian Diez, and Louis A. DeMore "Flight table orientation error transparency for hardware-in-the-loop facilities", Proc. SPIE 4366, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VI, (31 August 2001); https://doi.org/10.1117/12.438076

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