• Title/Summary/Keyword: measurement Noise

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Signal qualification method for high density disk (고밀도 디스크를 위한 신호 품질 평가 방법)

  • Park Hyun-Soo
    • Transactions of the Society of Information Storage Systems
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    • v.1 no.1
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    • pp.53-57
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    • 2005
  • In order to measure signal quality of optical disc such as CD or DVD, jitter is used traditionally. The signal attained from a disc by optical pick-up is processed by analog circuits. And then, binary signal can be obtained by using proper silcer. After the signal is changed into binary format, jitter is calculated as a time difference between the binary signal and the reference time. Jitter is used to express the signal quality. In this paper, a new method that is able to offer more precise measurement of the signal quality fur high density optical disc than the jitter is proposed. We named it LPSNR (Level Peak Signal to Noise Ratio). The relationship between bER (bit error rate) and LPSNR is shown in the paper.

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A Study on Parameter Estimation for General Aviation Canard Aircraft

  • Kim, Eung Tai;Seong, Kie-Jeong;Kim, Yeong-Cheol
    • International Journal of Aeronautical and Space Sciences
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    • v.16 no.3
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    • pp.425-436
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    • 2015
  • This paper presents the procedures used for estimating the stability and control derivatives of a general aviation canard aircraft from flight data. The maximum likelihood estimation method which accounts for both process and measurement noise was used for the flight data analysis of a four seat canard aircraft, the Firefly. Without relying on the parameter estimation method, several aerodynamic derivatives were obtained by analyzing the steady state flight data. A wind tunnel test, a flight test of a 1/4 scaled remotely controlled model aircraft, and the prediction of aerodynamic coefficients using the USAF Stability and Control Digital Data Compendium (DATCOM), Advanced Aircraft Analysis (AAA), and Computer Fluid Dynamics (CFD) were performed during the development phase of the Firefly and the results were compared with flight determined derivatives of a full scaled flight prototype. A correlation between the results from each method could be used for the design of the canard aircraft as well as for building the aerodynamic database.

Parameter estimation of a single turbo-prop aircraft dynamic model (단발 터어보프롭 항공기 동적 모델의 파라메터추정)

  • Lee, Hwan;Lee, Sang-Kee
    • Journal of Institute of Control, Robotics and Systems
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    • v.4 no.1
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    • pp.38-44
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    • 1998
  • The modified maximum likelihood estimation method is used to estimate the nondimensional aerodynamic derivatives of a single turbo-prop aircraft at a specified flight condition for the best deduction of the dynamic characteristics. In wind axes the six degree of freedom equations are algebraically linearized so that the linear state equation contains aerodynamic derivatives in a state-space form and is used in the maximum likelihood method. The simulated data added with the measurement noise is used as a flight test data which is necessary to the estimation of nondimensional aerodynamic derivatives. It is obtained by implementing the 6-DOF nonlinear flight simulation. In the flight simulation, the effects of several control input types, control deflection amplitudes, and the turbulence intensities on the statistical convergence criteria are also examined and quantitative analysis of the results is discussed.

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A Development of Waveform Composition Program and Evaluation of Application on Site (파형합성 프로그램 개발 및 현장 적용성 평가)

  • Yoon, Ji-Sun;Woo, Taek-Gyu;Bae, Sang-Hoon
    • Explosives and Blasting
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    • v.27 no.1
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    • pp.38-46
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    • 2009
  • Recently, as a reduction method of vibration and noise, an electronic detonation which has an accuracy of time and a freedom of input delay time was introduced. A waveform composition program can determine a delay time and accomplish simulation under environment similar to real blast using a delay time. In this study, optimum delay time which controls vibration is obtained and real measurement vibration level is estimated by a waveform composition program.

New Inchworm type Actuator with I/Q heterodyne Interferometer Feedback for a Long Stroke Precision Stage

  • Moon Chanwoo;Lee Sungho;Chung J.K
    • International Journal of Precision Engineering and Manufacturing
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    • v.6 no.2
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    • pp.34-39
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    • 2005
  • The precision stage is an essential device for optic fiber assembly systems, micro machines and semiconductor equipments. A new piezoelectric inchworm type actuator is proposed to implement an actuator-integrated long-stroke linear stage. An in-and-quadrature phase (I/Q) heterodyne interferometer is developed as a feedback sensor of a servo system, and a synchronized counting method is proposed. The proposed measurement system can measure the accurate position of fast moving object with robustness to external sensing noise from actuator vibration. The developed servo stage will be applied to optic fiber device assembly system.

Cam Design of Packer Holder in Egg Grading Machine (계란선별기 파커홀더 캠 개발)

  • Lee, Jang-Yong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.32 no.10
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    • pp.897-904
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    • 2008
  • Egg grading machine is used in poultry raising industry to classify eggs by their weight and to pack up them. Packer holder mechanism is a main part of the egg grading machine, of which role is to take eggs fallen from conveyor belt, and afterward to transfer eggs vertically to mold tray. The vertical motion of packer holder is usually driven by slider-crank mechanism or cam. This paper describes development of the cam in packer holder based on kinematic analysis of packer holder mechanism and measurement of acceleration and noise of the cam to verify performance of it. Several cams that are designed and manufactured by the author of this paper according to different design specification are compared to determine the best solution for egg transfer in the packer holder mechanism.

A Study on the Improvement of Finite Element Model for Scaled Frame by Considering Eigenvectors and Eigenvalues (고유벡터와 고유치를 고려한 모형 프레임의 유한요소 모델 개선에 관한 연구)

  • 김병곤;정태진;이종길;허덕재
    • Journal of KSNVE
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    • v.10 no.6
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    • pp.1009-1016
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    • 2000
  • This paper describes the procedure of increasing the efficiency of experimental modal analysis and updating the quality of FE model using the scaled commercial vehicle frame. In this study, it was found that the experimental modal analysis could be more efficient when the measurements were made on the areas with high kinetic energies. Such areas could be located with the aid of FE modal analysis. Also, the number of measurement points could be decided by considering the dynamic characteristics of full FE model. The correlation of FE model and experimental modal analysis was assessed by the differences between the natural frequencies and MAC matrix, which is based on normal modes. These differences of modal parameters were reduced through the sensitivity and optimization analysis of which objective function consisted of the errors of natural frequencies and the diagonal terms of MAC matrix.

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Development of a High Power SONAR System Measuring Velocity by Using Two Gated Sinusoidal Signals (두 개의 정현 신호를 이용한 속도 측정용 고전력 쏘나 시스템 개발)

  • 장순석;안흥구;이제형
    • Journal of KSNVE
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    • v.9 no.5
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    • pp.1036-1041
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    • 1999
  • This paper aims for the development of the high power sonar system for measuring the velocity of a moving object. The high power sonar system transmits two gated 190 kHz sinusoidal signals with 1.6 [ms] time interval to the moving object. Then the sonar system detects and calculates the changed time delay of the reflected ultrasonic signals in order to derive the velocity of the moving object. The transmission part uses a high power amplifier so that 250 W gated sinusoidal signals can be transmitted to the transmitter. 1M RAM is utilized for transmitting and storing of the ultrasonic signals. The time delay is calculted by the cross-correlation technique between the transmitted signals and the received signals. The measured value from the high power sonar system is compared with directly measured values by photo diodes. The result confirms the adjacency to 0.3% error.

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