kumoh national institute of technology
Networked Systems Lab.


NSL > Researches> Fieldbus> FieldBus
Flight Control System Architecture Development for A Small UAV Based on Field BUS(안정성이 검증된 필드버스인 CAN 을 이용하여 소형무인기의 비행제어 시스템 아키텍처를 구성한 연구사례)
By : 관리자
Date : 2015-08-25
Views : 632

This paper describes the flight control system interface architecture being developed for a high end small UAV. It emphasizes a small size, light weight, low cost and high reliability. This system employs Controller Area Network to reduce the size, weight and power consumption of the equipment in order to decrease the communication loads of the LRUs. It also achieved the cost saving. Control BUS secure a reliability by using dual and two channel communication BUS. The quality of the communication signals were verified with testing the eye-diagram of CAN.

자동차 및 로봇제어 분야에서 안정성이 검증된 필드버스인 CAN 을 이용하여 소형무인기의 비행제어시스템 아키텍처를 구성한 연구사례
- 비행제어 시스템의 메인 버스로서 필드버스의 적합성을 확인

관련 논문 : http://www.dbpia.co.kr/Journal/ArticleDetail/NODE06294897
(Total:29 articles / page:1/3 )
No. Subject By Date Views
29  Paper about filedbus in our laboratory ("Distribut.. 관리자 2018-10-31 16
28  Preparing the IIoT era by enhancing connectivity with .. 관리자 2018-07-25 50
27  Foundation Fieldbus Technology(1a.) 관리자 2018-06-26 59
26  Foundation Field-bus Technology(Learning and training .. 관리자 2017-09-04 311
25  Foundation Fieldbus Technology(4) 관리자 2017-07-10 436
24  Foundation Fieldbus Technology(3) 관리자 2017-07-03 435
23  Foundation Fieldbus Technology(2) 관리자 2017-06-19 403
22  Foundation Fieldbus Technology(1) 관리자 2017-04-24 550
21  Fieldbus diagnostic online solution program establishm.. 관리자 2017-04-17 427
20  EtherCAT Communication 관리자 2016-09-13 563