Abstract

Abstract : The Integrated Optical Diagnostics project integrated three optical diagnostics systems for use in the Aerodynamic 16-foot transonic wind tunnel testing area. Integration of the systems was provided through an optical diagnostics controller via fiber-optic reflective memory interface hardware. This hardware will be used as the common developmental structure for all future optical diagnostic techniques that will be used in the 16T environment. Control commands and data transfers from the 16T control/data system were accomplished through ethernet connection. This integration will provide aerospace system developers and testers the tools needed to reduce the total time required to conduct a wind tunnel test program.

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