PROCEEDINGS VOLUME 2840
SPIE'S 1996 INTERNATIONAL SYMPOSIUM ON OPTICAL SCIENCE, ENGINEERING, AND INSTRUMENTATION | 4-9 AUGUST 1996
Fly-by-Light III
IN THIS VOLUME

4 Sessions, 22 Papers, 0 Presentations
SPIE'S 1996 INTERNATIONAL SYMPOSIUM ON OPTICAL SCIENCE, ENGINEERING, AND INSTRUMENTATION
4-9 August 1996
Denver, CO, United States
FLASH I: Cable Plant
Proc. SPIE 2840, Aircraft optical cable plant: the physical layer for fly-by-light control networks, 0000 (14 October 1996); https://doi.org/10.1117/12.254210
Proc. SPIE 2840, Multifiber optical connectors for avionics, 0000 (14 October 1996); https://doi.org/10.1117/12.254220
Proc. SPIE 2840, Honeywell FLASH fiber optic motherboard evaluations, 0000 (14 October 1996); https://doi.org/10.1117/12.254225
Proc. SPIE 2840, Fiber optic connectors and splices for aircraft applications, 0000 (14 October 1996); https://doi.org/10.1117/12.254226
Proc. SPIE 2840, Smart skin array technology: a robust fiber optic approach, 0000 (14 October 1996); https://doi.org/10.1117/12.254227
FLASH II: Fly-by-Light Flight Control
Proc. SPIE 2840, FLASH fly-by-light flight control demonstration results overview, 0000 (14 October 1996); https://doi.org/10.1117/12.254228
Proc. SPIE 2840, Fly-by-light flight control system development for transport aircraft, 0000 (14 October 1996); https://doi.org/10.1117/12.254229
Proc. SPIE 2840, Demonstration results of fly-by-light flight control system architectures for tactical military aircraft, 0000 (14 October 1996); https://doi.org/10.1117/12.254230
Proc. SPIE 2840, Cost-efficient integrated tests of fly-by-light flight control systems, 0000 (14 October 1996); https://doi.org/10.1117/12.254231
Proc. SPIE 2840, On-board fault diagnostics for fly-by-light flight control systems using neural network flight processors, 0000 (14 October 1996); https://doi.org/10.1117/12.254211
FLASH III: Sensors and Components
Proc. SPIE 2840, Development of an optical fiber engine sensor suite, 0000 (14 October 1996); https://doi.org/10.1117/12.254212
Proc. SPIE 2840, Integration and test of a fiber optic gyro AHRS into a fly-by-light aircraft configuration, 0000 (14 October 1996); https://doi.org/10.1117/12.254213
FLASH II: Fly-by-Light Flight Control
Proc. SPIE 2840, Optical demonstration on Honeywell FLASH program, 0000 (14 October 1996); https://doi.org/10.1117/12.254214
FLASH III: Sensors and Components
Proc. SPIE 2840, FLASH fiber optic data bus lessons learned, 0000 (14 October 1996); https://doi.org/10.1117/12.254215
FBL Systems Technology
Proc. SPIE 2840, Fly-by-wire to fly-by-light issues and solutions, 0000 (14 October 1996); https://doi.org/10.1117/12.254216
Proc. SPIE 2840, Development of a laser wind and hazard profiler, 0000 (14 October 1996); https://doi.org/10.1117/12.254217
Proc. SPIE 2840, Design and certification of low-cost distributed Control-By-Light aircraft control systems for part 25 aircraft, 0000 (14 October 1996); https://doi.org/10.1117/12.254218
Proc. SPIE 2840, ASPEN: a multitransmitter, bidirectional fiber optic data bus designed for use in critical aircraft applications, 0000 (14 October 1996); https://doi.org/10.1117/12.254219
Proc. SPIE 2840, Distributed fiber optic sensor based on the Sagnac interferometer and fiber gratings for aircraft and spacecraft, 0000 (14 October 1996); https://doi.org/10.1117/12.254221
Proc. SPIE 2840, All-fiber double ring resonator using multiport coupler, 0000 (14 October 1996); https://doi.org/10.1117/12.254222
FLASH III: Sensors and Components
Proc. SPIE 2840, Long stroke optical fiber linear position sensor for the FLASH program, 0000 (14 October 1996); https://doi.org/10.1117/12.254223
Proc. SPIE 2840, Air data transducer with optical communications and an optical temperature sensor, 0000 (14 October 1996); https://doi.org/10.1117/12.254224
Back to Top