Paper
21 December 1978 An Optical Communication System For Aircraft
Thomas N. Rodgers
Author Affiliations +
Abstract
On many occasions it is required to modify a USAF aircraft to render it capable of supporting a Research, Development, Test and Evaluation (RDT&E) effort. This modification usually involves the addition of wires in the aircraft to gather and transmit data to an external instrumentation pod. This problem has limited the types of aircraft that could be modified to support tests and has been the cause for lengthy and expensive delays in test support. The Optical Communicator System (OCS) will minimize the previously mentioned problems and supply capabilities not now realizable. With the OCS, data is transmitted from the data source to the instrumentation pod via a modulated, non-coherent light beam. The OCS is capable of handling 140 independent, simultaneous data channels under realistic airborne environmental conditions. Features of the system include: visible light beam utilized for alignment, a memory to assure logical data output at all times; a "test word" to assure optical path integrity while in-flight; sufficient system beamwidth to allow for relative motion between the instrumentation pod on the aircraft wing and the data initia-tion point. The OCS is completing airborne acceptance testing at this time.
© (1978) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Thomas N. Rodgers "An Optical Communication System For Aircraft", Proc. SPIE 0150, Laser and Fiber Optics Communications, (21 December 1978); https://doi.org/10.1117/12.956706
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KEYWORDS
Telecommunications

Optical communications

Transmitters

Light emitting diodes

Receivers

Analog electronics

Data communications

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