DocumentCode :
2592953
Title :
Assessment of photonics for advanced integrated avionics processors-PAVE PACE
Author :
Allyn, Christopher L. ; Hummel, Edward M. ; Pimpinella, Richard J.
Author_Institution :
AT&T Bell Lab., Whippany, NJ, USA
fYear :
1990
fDate :
15-18 Oct 1990
Firstpage :
289
Lastpage :
292
Abstract :
It is suggested that advanced photonics offers major benefits to next-generation military avionics in terms of performance, reliability, and cost-effectiveness. The trends in photonic technologies are discussed, and their applicability for use in integrated avionics systems is assessed. Optical switching, interconnection, and processing are discussed, as well as the potential benefits to advanced architectures such as PAVE PACE. It is concluded that the movement and management of large amounts of data in upcoming systems will not be possible without optics. The major impact will be the widespread use of fiber transmission and optical switching. It is expected that advanced photonic technology for, sensors and system networking (e.g. fly-by-light and smart structures and skins) will also support important improvements in platform performance
Keywords :
aerospace computing; aircraft instrumentation; computer architecture; economics; fibre optic sensors; fibre optics; military equipment; optical interconnections; optical switches; reliability; PAVE PACE; advanced integrated avionics processors; cost-effectiveness; fiber optic sensors; fiber transmission; fly-by-light; military avionics; optical interconnection; optical switching; photonics; reliability; skins; smart structures; Aerospace electronics; Intelligent sensors; Intelligent structures; Optical fiber sensors; Optical interconnections; Optical sensors; Optoelectronic and photonic sensors; Potential well; Sensor systems; Skin;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location :
Virginia Beach, VA
Type :
conf
DOI :
10.1109/DASC.1990.111301
Filename :
111301
Link To Document :
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