• 제목/요약/키워드: Pitch

검색결과 4,262건 처리시간 0.031초

Peak 검출과 AMDF에 의한 고속도 음성주기 추출방법 (A High Speed Pitch Extraction Method Based on Peak Detection and AMDF)

  • 성원용;은종관
    • 대한전자공학회논문지
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    • 제17권4호
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    • pp.38-44
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    • 1980
  • 본 논문에서는 peak 검출과 average magnitude difference function (AMDF)방법을 이용해서 음성의 주기를 고속도로 추출하는 방법이 연구되었다. 먼저 입력 음성을 800Hz로 대역폭을 줄인다음 Pitch peak가 될 만한 몇개의 Peak을 검출한다. 그 다음 이들 peak들의 값을 갖고 AMDF를 계산해서 이들 값들 중에서 최소의 AMDF치를 갖는 peak를 원하는 음성주기로 결정을 한다. 이 방법을 사용하여 음성의 주기를 검출하면 타 음성주기 추출방법 보다 훨씬 적은 계산 시간이 소요될 분만 아니라 비교적 정확한 결과를 얻을 수 있다.

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풍력터빈 축 진동 응답에 대한 피치 게인-스케쥴링의 효과 (An Effect of Pitch Gain-Scheduling on Shaft Vibration Response of Wind Turbine)

  • 임채욱;조준철
    • 한국유체기계학회 논문집
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    • 제15권2호
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    • pp.36-40
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    • 2012
  • Pitch control of wind turbine is activated above rated wind speed for the purpose of rated power regulation. When we design pitch controller, its gain-scheduling is essential due to nonlinear characteristics of aerodynamic torque. In this study, 2-mass model including a vibration mode of drive-train for a 2 MW wind turbine is considered and pitch control with gain-scheduling using a linearization analysis of the nonlinear aerodynamic torque is applied. Some simulation results for the pitch gain-scheduling under step wind speed are presented and investigated. It is shown that gain-scheduling in pitch control is important especially in the region of high wind speeds when there exists a vibration mode of drive-train.

무베어링 헬리콥터 주 로터의 허브 파라미터 변화에 따른 로터 안정성 특성 해석 (Hub Parametric Investigation of Main Rotor Stability of Bearingless Helicopter)

  • 윤철용;기영중;김태주;김덕관;김승호
    • 한국소음진동공학회논문집
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    • 제22권8호
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    • pp.784-790
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    • 2012
  • This paper describes a stability and dynamic characteristics of bearingless helicopter main rotor in hover. Baseline rotor configuration is defined and modal analysis for the configuration is taken to verify the dynamic characteristics. The kinematic pitch-lag couplings through ways of pitch link installation are analyzed to know effects on loads, frequencies and stability. The effects of pitch link attachments in spanwise direction and chordwise direction as well as pitch link inclination on thrust, power, flpa-lag-pitch mode frequencies and inplane damping are examined. Pitch link at trailing edge location in chordwise direction has influence on aeroelastic stability of the rotor. Also, the pitch link with negative inclination angle makes inplane damping increase.

중국인 학습자들의 한국어 낭독 문장 피치곡선의 변동 양상 (A Study on the Pitch Contour Variation in Reading Sentence Produced by Chinese Korean-Learners)

  • 윤영숙
    • 말소리와 음성과학
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    • 제5권2호
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    • pp.59-69
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    • 2013
  • The purpose of this study is to examine the variation of pitch contour observed in the reading of Korean sentences produced by Chinese Korean-learners. In the reading context, Korean sentence intonation can be described by considering accentual phrases' pitch pattern and intonational phrases' boundary tone. But when APs and IPs connect to each other to form sentences, another aspect of speech production must be considered, that is declination of pitch contour. So, in order to examine how Chinese speakers produce Korean sentence intonation, we have analysed the sentences' pitch contours produced by fourteen Chinese speakers differing in proficiency, and compared them to pitch contours produced by six Korean native speakers. The results show that Chinese speakers tend to decline the pitch contour in shorter sentences, but for longer sentences, the declination was not observed. Moreover, even though Chinese speakers produced sentences with declination, internal tonal modulation differs from native speakers.

무베어링 헬리콥터 주 로터의 허브 파라미터 변화에 따른 로터 안정성 특성 해석 (Hub Parametric Investigation of Main Rotor Stability of Bearingless Helicopter)

  • 윤철용;기영중;김태주;김덕관;김승호
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2012년도 춘계학술대회 논문집
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    • pp.394-399
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    • 2012
  • This paper describes a stability and dynamic characteristics of bearingless helicopter main rotor in hover. Baseline rotor configuration is defined and modal analysis for the configuration is taken to verify the dynamic characteristics. The kinematic pitch-lag couplings through ways of pitch link installation are analyzed to know effects on loads, frequencies and stability. The effects of pitch link attachments in spanwise direction and chordwise direction as well as pitch link inclination on thrust, power, flpa-lag-pitch mode frequencies and inplane damping are examined. Pitch link at trailing edge location in chordwise direction has influence on aeroelastic stability of the rotor. Also, the pitch link with negative inclination angle makes inplane damping increase.

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개별 피치정보를 이용한 멀티펄스 음성부호화 방식에 관한 연구 (A Study on Multi-Pulse Speech Coding Method by Using Individual Pitch Information)

  • 이시우
    • 한국콘텐츠학회논문지
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    • 제6권2호
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    • pp.59-64
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    • 2006
  • 본 연구에서는 피치추출 오류를 줄이고 피치간격의 변위에 적응할 수 있도록 피치간격을 정규화하지 않은 개별피치 펄스를 이용한 새로운 멀티펄스 음성부호화 방식(IP-MPC)을 제안하였다. 여기에서, 개별피치 펄스의 추출률은 남자음성에서 $96\%$, 여자음성에서 $85\%$를 얻을 수 있었으며, 개별피치 펄스를 이용한 IP-MPC와 자기상관법의 피치정보를 이용한 MPC를 평가한 결과, IP-MPC의 음질이 MPC의 음질에 비하여 상당히 개선되었음을 알 수 있었다.

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피치제어형 풍력발전시스템의 출력제어 (Power Control of a Pitch-controlled Wind Power System)

  • 임종환;허종철
    • 한국정밀공학회지
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    • 제20권4호
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    • pp.84-91
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    • 2003
  • The paper presents a power control algorithm for a full pitch-controlled wind power system. The design of a pitch controller, in general, is performed by linearizing the torque in the vicinity of a operating point assuming the tip speed ratio is constant. For power control, however, the tip speed ratio is no longer a constant. In this study, a reference pitch model is derived in terms of a wind speed, angular velocity, and pitch angle. The reference pitch model is used to design a controller without linearizing the non-linear torque model of the blade. The validity of the algorithm is demonstrated with the results produced through sets of simulation.

피치제어형 풍력발전시스템의 속도제어 (Speed Control of a Wind Turbine System Based on Pitch Control)

  • 임종환;허종철
    • 제어로봇시스템학회논문지
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    • 제7권2호
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    • pp.109-116
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    • 2001
  • The paper presents a speed control algorithm for a full pitch-controlled wind turbine system. Torque of a blade generated by wind energy is a nonlinear function of wind speed, angular velocity, and pitch angle of the blade. The design of the controller, in general, is performed by linearizing the torque in the vicinity of the operating point assuming the angular velocity of the blade is constant. For speed control, however the angular velocity is on longer a constant, so that linearization of the torque in terms of wind speed and pitch angle is impossible. In this study, a reference pitch model is derived in terms of a wind speed, angular velocity, and pitch angle, which makes it possible to design a controller without linearizing the nonlinear torque model of the blade. This paper also suggests a method of designing a hydraulic control system for changing the pitch angle of the blade.

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Optimization of a four-bar mechanism cyclic pitch control for a vertical axis wind turbine

  • Montenegro-Montero, Mariana;Richmond-Navarro, Gustavo;Casanova-Treto, Pedro
    • Wind and Structures
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    • 제35권2호
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    • pp.121-130
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    • 2022
  • In this paper, the issue of pitch control in a vertical axis wind turbine was tackled. Programming the Actuator Cylinder model in MATLAB, a theoretical optimum pitch solution was found and then a classic four-bar mechanism was adapted to that theoretical solution to achieve a simple and elegant control of the pitch in the turbine. A simulation using the mechanism worked to find the optimum pitch cycles, where it was found that the mechanism would, in fact, increase the efficiency of the VAWT, by at least 11% and in the best case, over 35%. Another aspect that is studied is the possibility of self-start of the turbine by only changing the pitch on the blades. This analysis, however, proved that a further individual pitch control must be used to surpass the cogging torque. All analyses conducted were done for a specific wind turbine that is 2 m2 in the swept area.

실시간 SIFT 기본주파수 검출기의 구현 (Implementation of a Real-time SIFT Pitch Detector)

  • 이종석;이상욱
    • 대한전자공학회논문지
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    • 제23권1호
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    • pp.101-113
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    • 1986
  • In this paper, a real-time pitch detector LPC vocoder as implemented on a high speed digital signal processor, NEC 7720, is described. The pitch detector was based mainly on the SIFT algorithm. The SIFT pitch detector consists primarily of a digital low pass filter, inverse filter, computation of autocorrelation, a peak picker, interpolation, V/UV defcision and a final pitch smoother. In our approach, modification, mainly on the V/UV decision and a final pitch smoother, was made to estimate more accurate pitches. An 16-bit fixed-point aithmatic was employed for all necessary computation and the simulated results were compared with the eye detected pitches obtained from real speech data. The pitch detector occupies 98.8% of the instruction ROM, 37% of the data ROM, and 94% of internal RAM and takes 15.2ms to estimate a pitch when an analysis frame is consisted of 128 sampled speech data. It is observed that the tested results were well agreed with the computer simulation results.

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