Fiber optic systems for mobile platforms II: 6-7 September 1988, Boston, Massachusetts
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AUTOMOTIVE FIBER OPTIC APPLICATIONS
SPACECRAFT LAUNCH AND MISSILE SYSTEMS
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aircraft applications avionics bandwidth bypass cable circuit coherence length components configuration connection connector control systems core cost counter-rotating ring data bus data rate datalink detector developed device diameter diode distribution division multiplex electrical electro-optic electronics environment environmental FDMA fiber optic sensor fiber optic systems fiber-optic fluorescent frequency function hardware input insertion loss installation interface laser laser diode launch light source linear macrobending sensor maximum measured mechanical missile Mobile Platforms modal mode modulation modulation index monitoring multimode node operation optic multiplex optic switches optical fiber optical power output parameters payout performance photodiode polymer fiber position sensor power budget pulse range ratio receiver reliability SAFENET sensor system shown in Figure signal simulation Space Station star coupler step index fiber subsystem TDIN technique temperature thermo-setting topology transducer transmission transmitted vehicle waveguide wavelength wavelength division multiplexing