• 한국조명전기설비학회:학술대회논문집
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• 한국조명전기설비학회 2004년도 학술대회 논문집
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• pp.365-370
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• 2004

The integration of intelligent devices, devices-level networks, and software into motor control systems can deliver improved diagnostics, fast warnings for increased system reliability, design flexibility, and simplified wiring. Remote access to motor-control information also affords an opportunity for reduced exposure to hazardous voltage and improved personnel safety during startup and trouble-shooting. This paper presents LonWorks fieldbus networked intelligent induction control system architecture. Experimental bed system with two inverter motor driving system for controlling 1.5kW induction motor is configured for LonWorks networked intelligent motor control. In recent years, MCCs have evolved to include component technologies, such as variable-speed drives, solid-state starters, and electronic overload relays. Integration was accomplished through hardwiring to a programmable logic controller (PLC) or distributed control system (DCS). Devicelevel communication networks brought new possibilities for advanced monitoring, control and diagnostics. This LonWorks network offered the opportunity for greatly simplified wiring, eliminating the bundles of control interwiring and corresponding complex interwiring diagrams. An intelligent MCC connected in device level control network proves users with significant new information for preventing or minimizing downtime. This information includes warnings of abnormal operation, identification of trip causes, automated logging of events, and electronic documentation. In order to show the application of the multi-motors control system, the prototype control system is implemented. This paper is the first step to drive multi-motors with serial communication which can satisfy the real time operation using LonWorks network.

• 한국항공우주학회지
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• 제42권5호
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• pp.406-414
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• 2014

본 논문에서는 한국형기동헬기에 탑재된 FMCW형 레이더고도계의 특성에 대해 소개하고 비행시험 및 지상기능점검 중 발생한 레이더고도계의 결함에 대해 기술하였다. 또한 효율적이고 적시적인 결함 분석과 설계개선안 도출을 위해 데이터/제어흐름 모델을 기반으로 결함요인을 분석하고 설계개선안에 대해 시스템 통합 실험과 비행시험으로 검증하였다. 레이더고도계 단품 및 항공기 체계에 대한 검증결과 결함 해소를 확인하였으며 이를 통해 항공기 안전성과 작전수행능력을 향상시켰다.