• Title/Summary/Keyword: 스위칭 함수 생성기

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The Construction of the Digital Logic Switching Functions using PLA (PLA에 기초한 디지털논리스위칭함수 구성)

  • Park, Chun-Myoung
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.12 no.10
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    • pp.1794-1800
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    • 2008
  • This paper presents a method of constructing the digital logic switching functions using PLA. First of all, we propose a MIN and MAX algebra arithmetic operation based on the Post algebra. And we discuss the T-gate which is used for realization of the MIN and MAX algebra arithmetic operation. Next, we discuss the MIN array and MAX array which are basic circuit of the PLA, also we discuss the literal property. For the purpose of the design for the digital logic switching functions using PLA, we Propose the variable partition, modular structure design, literal generator, decoder and invertor. The proposed method is the more compactable and extensibility.

Model of Remote Service and Intelligent Fault Diagnosis for CNC Machine Tool (공작기계의 지능형 고장진단과 원격 서비스 모델)

  • Kim, Sun-Ho;Kim, Dong-Hoon;Han, Gi-Sang;Kim, Chan-Bong
    • Journal of the Korean Society for Precision Engineering
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    • v.19 no.4
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    • pp.168-178
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    • 2002
  • The CNC machine toots has two kinds of fault. One is the fault due to degraded parts and the other is the fault due to operation disability. The phenomena of degradation is predictable but the operational fault is unpredictable because it occurred without any warning. The major faults of CNC machine tool are operational faults which are charged over 70%. This paper describes the model of remote service and the intelligent fault diagnosis system to diagnosis operational faults of CNC machine tools. To generalize fault diagnosis, two diagnosis models such as SF(Switching Function) and SSF(Step Switching Function) are proposed. The SF is static model and SSF is dynamic model for expression of fault. The SF and SSF model can be generated using SFG(Switching Function Generator) which is developed in this research. The three major operational faults such as emergency stop error, cycle start disability and machine ready disability are applied to experiment of fault modeling. To remote service of faults fur CNC machine tool, the web server and client system based internet are proposed as the suitable environment. The developed two technologies are implemented with the internal function of open architecture controller. The implemental results for two technologies are presented to validate the proposed scheme.

Modeling and Line Current Control of a Three Phase Voltage Source Inverter using an LCL filter in a Balanced Delta Circuit (LCL 필터를 사용하는 삼상 전압형 인버터의 모델링과 계통전류 제어)

  • Lee, Sang-In;Lee, Kui-Jun;Hyun, Dong-Seok
    • Proceedings of the KIPE Conference
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    • 2007.11a
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    • pp.18-20
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    • 2007
  • 3상 계통 연계 형 인버터 시스템은 낮은 THD를 가지는 계통 전류를 공급해주기 위해 LCL 필터를 사용한다. LCL 필터를 사용하는 가장 큰 장점은 낮은 스위칭 주파수에서도 만족할 만한 수준의 THD를 가지는 계통 전류를 생성시킬 수 있다는 점이다. 반면에, 단점은 LCL필터를 포함하는 계통 연계 형 인버터 시스템의 전달함수에 하나의 공진 극점이 존재한다는 점이다. 이것은 계통 전류 제어 loop에서, 안정성 문제에 영향을 미친다. 정확한 제어를 위해서 시스템의 전달함수는 필수적이다. 여기서 중요한 점은 많은 저자들이 시뮬레이션과 실험을 할 때, 중성점이 없는 회로에서 행하지만 회로 해석을 할 때에는 중성점이 있는 회로에서 해석을 한다는 점이다. 그래서 우리는 등가 델타회로에서 LCL 필터를 포함한 전체 시스템의 수학적인 모델을 제안한다. 이 모델은 모든 인덕터와 커패시터의 기생 저항을 고려한다. 또한 이 논문은 계통 전류를 제어하기 위한 제어기의 해석적인 설계 절차를 포함한다. 제안한 수학적인 모델을 입증하기 위해, PSIM을 통한 시뮬레이션과 Simulink를 통한 시뮬레이션 결과를 비교하였다.

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Integrated Simulation of Descent Phase using the RCS jet for a Lunar Lander (RCS jet을 고려한 달착륙선의 Descent phase 통합 시뮬레이션)

  • Min, Chan-Oh;Jeong, Seun-Woo;Lee, Dae-Woo;Cho, Keum-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.6
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    • pp.473-480
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    • 2013
  • Researches for various lunar landing technologies are in progress for the lunar exploration program planned for early 2020s in Korea. This paper shows the integrated simulation for safe lunar landing guidance/control system in powered descent phase. Generally, the lunar lander uses on/off(bang-bang) controller to control the RCS jet thrusters instead of proportional controller. In this paper, the on/off controller using phase-plane switching function, and thruster selection algorithm to control sixteen thrusters are applied. Also additional guidance commands are calculated by a proposed fuzzy logic guidance algorithm. The simulation results show that lunar lander can follow a reference trajectory which is generated by optimization method, then land on the surface safely.