DocumentCode :
2488647
Title :
The power by wire and optical data bus prototype system integration
Author :
Yokota, Masahiko ; Shinoda, Naomasa ; Yamaba, Katsushi ; Nakagawa, Norio ; Nagato, Toshba
Author_Institution :
Kawasaki Heavy Ind. Ltd., Gifu, Japan
Volume :
2
fYear :
2002
fDate :
2002
Abstract :
We have studied a power-by-wire/fly-by-light (PBW/FBL) system for years and developed prototype equipment such as an optical data bus, electric smart actuator and flight control computer. The optical data bus includes commercial based single mode fiber, optical couplers and E/O (electro/optical) transceiver that is small enough to be installed inside each piece of electronic equipment. The electric smart actuator is a triple redundant 270 V DC EMA (electro mechanical actuator) package with embedded control electronics. Also, a new fault detection and reconfiguration capability was demonstrated using the flight control computer prototype. The functional test and environmental test for each component are almost completed. Currently, we are starting the system integration bench test in which all prototype equipment will be connected using the optical data bus. We present the prototype design, equipment test results and system integration test plan.
Keywords :
aircraft computers; aircraft control; aircraft power systems; electric actuators; electro-optical devices; fault location; intelligent actuators; optical fibre communication; optical fibre couplers; 270 V; E/O transceivers; PBW/FBL; aircraft power-by-wire/optical data bus systems; electric smart actuators; electro mechanical actuators; electro/optical transceivers; embedded control electronics; flight control computer fault detection/reconfiguration; optical couplers; power-by-wire/fly-by-light systems; single mode fibers; system integration; triple redundant EMA; Aerospace control; Integrated optics; Intelligent actuators; Optical computing; Optical fiber couplers; Optical fiber devices; Prototypes; System testing; Transceivers; Wire;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 2002. Proceedings. The 21st
Print_ISBN :
0-7803-7367-7
Type :
conf
DOI :
10.1109/DASC.2002.1053005
Filename :
1053005
Link To Document :
بازگشت