• 제목/요약/키워드: carrier space

검색결과 371건 처리시간 0.021초

An Improved Carrier-based SVPWM Method By the Redistribution of Carrier-wave Using Leg Voltage Redundancies in Generalized Cascaded Multilevel Inverter

  • Kang, Dae-Wook;Lee, Yo-Han;Suh, Bum-Seok;Park, Chang-Ho;Hyun, Dong-Seok
    • Journal of Power Electronics
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    • 제1권1호
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    • pp.36-47
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    • 2001
  • The carrier-based space vector pulse width modulation(SVPWM), which is considered as highly simple and efficient PWM technology, can be also used in multilevel inverters. The method was originally designed for the two-level inverter and developed to the diode clamped multilevel inverter structure. however it may be noted that it also cause bad switch utilization in cascaded multilevel inverter. This paper introduces an improved carrier-based SVPWM scheme, which is fully suitable for cascaded multilevel inverter topologies because it can achieve the optimized switch utilization through the redistribution of the triangular carrier waves considering leg voltage redundancies while having the advantages of the conventional carrier-based SVPWM. Using simulation and experimental results, the superior performance of new PWM method is shown.

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GPS 반송파 위상변화율을 이용한 SDINS/GPS 복합항법 필터 구성 (Study on SDINS/GPS Kalman Filter using GPS carrier phase rate measurements)

  • 박준구
    • 한국항공우주학회지
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    • 제34권11호
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    • pp.42-46
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    • 2006
  • SDINS 운항중 정렬에 적용 가능한 GPS 반송파 위상변화율 측정 모델을 유도하여 새로운 SDINS/GPS 복합항법 시스템 구성 방법을 제안한다. 제안된 SDINS/GPS 복합항법 필터의 성능 분석을 공분산 해석기법을 이용하여 수행하고 이의 결과를 실제 차량 실험을 통하여 검증한다. 제안된 결합기법은 2개 이상의 안테나를 갖는 SDINS/GPS 결합시스템에 적용가능하며 기수각 추정에 직접적으로 연계된 GPS 측정치를 생성함으로써 빠른 SDINS의 기수각 추정을 가능하게 함으로써 SDINS/GPS의 항법 성능을 향상시키게 된다.

기저선 제한조건을 이용한 GPS 반송파 바이어스 오차의 검출확률 향상 (Detection Probability Improvement of Bias Error of GPS Carrier Measurement using Baseline Constraint)

  • 이은성;천세범;이영재;강태삼;지규인
    • 한국항공우주학회지
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    • 제32권9호
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    • pp.88-93
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    • 2004
  • 본 논문에서는 기저선 제한조건을 이용하여 GPS 반송파 측정값에 바이어스 존재 여부를 보다 정확하게 판단하는 방법을 확인하고, 시뮬레이션을 통하여 이를 분석하였다. 기저선 제한조건은 추가적인 측정값으로 사용되며, 기존의 GPS 반송파 측정 방정식을 확장하는 형태로 사용된다. GPS 반송파 측정값만을 사용하는 경우와 기저선 제한조건을 함께 사용하는 경우에 대하여, 각각 검출확률(Detection Probability)를 계산하고 기저선 제한조건을 사용하는 경우 검출확률이 향상되는 것을 보이게 된다. 기저선 제한조건을 사용하는 것에 대한 장점을 통계적으로 증명하고 시뮬레이션을 통하여 수치적인 결과를 확인한다.

라이시안 페이딩 채널에서 공간 다이버시티를 적용한 Pilot Symbol Assisted Multi-Carrier CDMA BPSK 시스템의 성능 분석 (Performance Analysis of Pilot Symbol Assisted Multi-Carrier CDMA BPSK System with Space Diversity in Rician Fading Channels)

  • 노재성;오창헌;김언곤;조성준
    • 한국통신학회논문지
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    • 제26권6A호
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    • pp.913-922
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    • 2001
  • Multi-Carrier CDMA 시스템에서 불완전한 채널 예측과 다중사용자 간섭은 시스템의 성능 저하를 유발한다. 본 논문에서는 역방향 링크에서 파일럿 심볼을 이용하여 채널을 예측하는 Multi-Carrier CDMA BPSK 시스템에서 불완전한 채널 예측과 다중사용자 간섭의 영향을 연구하였다. 더욱이, 라이시안 페이딩 채널의 역방향 링크에서 최대비 합성 공간 다이버시티와 선택 합성 공간 다이버시티 기법을 적용한 성능 개선에 대하여 연구하였다. 수치계산 결과, 파일럿 심볼을 이용하여 채널을 예측하는 Multi-Carrier CDMA BPSK 시스템의 BER 성능은 등가 잡음 대역폭의 분산($\sigma$$^2$$_{c}$)에 매우 민감하나 무선 채널에서의 신호 전력 대 잡음 전력비에는 그리 심하지 않았다. 불완전한 채널 예측에 의한 BER 열화와 파일럿 심볼 간격의 최적화는 라이시안 페이딩 채널에서 Multi-Carrier CDMA BPSK 시스템의 BER 계산을 통하여 얻을 수 있었다. 그리고 불완전한 채널 예측에 의한 BER 열화는 신호 전력 대 잡음 전력비와 채널 예측 필터의 등가 잡음 대역폭에 관계하고 있음을 알 수 있었다.

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Analysis of the Flow Field of Carrier-Based Aircraft Exhaust Jets Impact on the Flight Deck

  • Yue, Kuizhi;Sun, Yicheng;Liu, Hu;Guo, Weigang
    • International Journal of Aeronautical and Space Sciences
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    • 제16권1호
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    • pp.1-7
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    • 2015
  • In order to provide some references for suitability of carrier-based aircrafts, this paper studies the flow field of exhaust jets and its impact on the flight deck. The geometrical models of aircraft carrier and carrier-based aircrafts are firstly built, on which unstructured tetrahedral meshes are generated for numerical analysis. Then, this paper simulates the flow field of exhaust jets to evaluate its impact on the Jet Blast Deflector (JBD) and the flight deck, when four carrier-based aircrafts are ready to start off in the bow. The standard k-${\varepsilon}$ equations, three-dimension N-S equations and the Computational Fluid Dynamics (CFD) theory are used in the analysis process. To solve the equations, the thermal coupling of the wind and the jet flow are also considered. The velocity and temperature distributions are provided with the simulation of the CFD software, FLUENT. The results indicate that: (1) this analytical method can be used to simulate aerodynamic problems with complex geometrical models, and the results are of high reliability; (2) the safety working area, the installation scheme of the JBD and the arrangement of the take-off position can be optimized through analysis.

Precision Orbit Determination of the SAC-C Satellite Using the GPS Dual Frequency Measurement

  • Yoon, Jae-Cheol;Im, Jeong-Heum;Moon, Hong-Youl;Lee, Sang-Ryool;Lee, Byoung-Sun
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2003년도 한국우주과학회보 제12권2호
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    • pp.48-48
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    • 2003
  • A precision orbit determination (POD) system of low Earth orbiter using the GPS dual frequency measurements has been developed. It is an option of KOMPSAT-2 POD process system. In this research, the orbit determination using the real dual frequency carrier phase measurements of the SAC-C satellite was conducted to verify KOMPSAT-2 POD system reliability. The SAC-C satellite is an international cooperative mission between NASA, the Argentine Commission on Space Activities (CONAE), Centre National d'Etudes Spatiales (CNES or the French Space Agency), Instituto Nacional De Pesquisas Espaciais (Brazilian Space Agency), Danish Space Research Institute, and Agenzia Spaziale Italiana (Italian Space Agency). The SAC-C was launched at November 21, 2000. The altitude of SAC-C is 702 km and it carries a TurboRogue III GPS and four high gain antennas developed by the JPL. The receiver is able to generate the dual frequency code and carrier phase data. Double-differenced carrier phase measurements were formed using 25 IGS stations. The data were sampled at 30 seconds interval. Fully dynamic approach was adopted for POD. The POD results were compared with those of JPL using GOA n software. The comparison verifies that deci-meter level 3D position accuracy of low Earth orbiting satellite could be achieved. The POD system has been developed successfully.

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Random PWM 기법을 이용한 무정전 전원장치의 노이즈 저감에 관한 연구 (A study on the Noise Reduction of Uninterruptible Power Supply using Random PWM Method)

  • 엄태욱;이병순;이재학
    • 조명전기설비학회논문지
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    • 제28권11호
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    • pp.100-105
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    • 2014
  • In this paper, Uninterruptible Power Supply(UPS) Inverter system using Carrier Frequency Modulated PWM (CFM-PWM) is proposed to reduced harmonics and electromagnetic noise. Power conversion of UPS system is executed by the ON-OFF operation of semiconductor switching devices. However, this switching operation causes the surge and EMI which deteriorate the reliability of the UPS system. This Problems improved by Random PWM switching method. The simulation results of the proposed system was compared with the system using conventional method using Matlab/Simulink. The results show that the output voltage and current harmonics of the proposed UPS system significantly decreased and spread into wide band area by the proposed Carrier Frequency Modulated PWM(CFM-PWM) method based on the Space Vector Modulation.

Voltage Source Inverter Drive Using Error-compensated Pulse Width Modulation

  • Chen, Keng-Yuan;Hu, Jwu-Sheng;Lin, Jau-Nan
    • Journal of Power Electronics
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    • 제16권1호
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    • pp.388-397
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    • 2016
  • An error-compensated pulse width modulator (ECPWM) is proposed to improve the baseband harmonic performance and the switching loss of voltage source inverters (VSIs). Selecting between harmonic distortion and switching loss is a design tradeoff in the conventional space vector pulse width modulation. In this work, an accumulated difference in produced and desired phase voltages is considered to adjust the reference signal. This mechanism can compensate for the voltage error in the previous carrier period. With error compensation every half-carrier period, the proposed ECPWM allows one-half reduction in carrier frequency without scarifying baseband harmonic distortion. The proposed modulator is applied to a three-phase VSI with R-L load and a motor-speed-control system for experiments. The measured efficiency and operating temperature of switches confirm the effectiveness of the proposed scheme.