• Title/Summary/Keyword: linear interpolator

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An universal NURBS interpolator for an architectured CNC controller (개방형 수치제어 장치를 위한 범용 NURBS 보간기)

  • 강성균
    • 제어로봇시스템학회:학술대회논문집
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    • 1996.10b
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    • pp.656-659
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    • 1996
  • An universal NURBS interpolation for an open architectured CNC controller is proposed in order to unify internal data structure and algorithm of different interpolations such as linear, circular and spline, and to intelligently interface CAD database of the various workpiece contour. Furthermore, NURBS interpolation may result in better surface roughness and high speed machining due to the continuous generation of cutter movement. The mathematical manipulation of NURBS is presented and the practical implementation on the CNC controller of a lathe is discussed for real machining. The comparison between a computer design and workpieces machined on a lathe shows the feasibility of the NURBS interpolation format as an universal interpolation scheme.

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The Oscillation Frequency of CML-based Multipath Ring Oscillators

  • Song, Sanquan;Kim, Byungsub;Xiong, Wei
    • JSTS:Journal of Semiconductor Technology and Science
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    • v.15 no.6
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    • pp.671-677
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    • 2015
  • A novel phase interpolator (PI) based linear model of multipath ring oscillator (MPRO) is described in this paper. By modeling each delay cell as an ideal summer followed by a single pole RC filter, the oscillation frequency is derived for a 4-stage differential MPRO. It is analytically proved that the oscillation frequency increases with the growth of the forwarding factor ${\alpha}$, which is also confirmed quantitatively through simulation. Based on the proposed model, it is shown that the power to frequency ratio keeps constant as the speed increases. Running at the same speed, a 4-stage MPRO can outperform the corresponding single-stage ring oscillator (SPRO) with 27% power saving, making MPRO with a large forwarding factor ${\alpha}$ an attractive option for lower power applications.

Design of NC Controller with personal computer (PC를 이용한 NC 장치의 설계)

  • Chung, G.J.;Kim, I.H.;Kang, Y.K.
    • Proceedings of the KIEE Conference
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    • 1988.07a
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    • pp.971-974
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    • 1988
  • In this study, we designed a model of NC controller with IBM-PC as a host CPU and intelligent servo controller for 2 axes that can be expaned to 4 axes. OS software was developed with C language at the base of mode selection technic for 9 NC operating modes. Servo controller design was based on the application of interpolator IC(3701) and position controller IC(3702) that permits low cost and high performance. For connection of two systems, parallel I/O communication was implemented. Finally, auto interpolation program test was executed for linear and circular paths resulting 1 LSB accuracy.

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The Method for Removing Jagging Artifact (Jagging Artifact 억제 기법)

  • Yang Seoung-Joon;Lee In-Hwan;Kwon Young-Jin
    • The Transactions of the Korean Institute of Electrical Engineers D
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    • v.54 no.3
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    • pp.194-197
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    • 2005
  • Digital display products are gradually becoming diversified and pursuing high-quality image display. Digital TV supports various video signal formats from conventional SD to digital HD because the format conversion of video image is required. Traditional format conversion of the video image is achieved by a 1-dimensional linear interpolator applying both horizontal and vertical direction. Jagging artifact can be expressed as the linkage of line segments in several directions. In this paper, we present the method that removes jagging artifact effectively using PCA (Principle Component Analysis) and reserve the detail in a given image.

Design of a 2-axis interpolator using FPGA (FPGA를 이용한 2축 보간기의 설계)

  • Yeo, Su-Jin;Kim, Jong-Eun;Won, Jong-Baek;Park, Jong-Sik
    • Proceedings of the KIEE Conference
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    • 2003.11c
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    • pp.596-599
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    • 2003
  • In this paper, we designed the digital pulse motor control chip including a circular interpolation function. The proposed algorithm in this paper is a nonparametric cure generation algorithm (Jordan's algorith) and a very simple algorithm. So the design for this algorithm used a small number of gates. Also an average error is fairly low. The max output speed is 4Mpps(Pulse per second), the max input frequency is 16MHz and the chip is useful for the stepping and servo motors. The software contains one or two, and many axes linear interpolation algorithm and two axes circular interpolation algorithm.

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Development of Software Interpolators for PC-based NC Machine Tools (PC-based NC 공작기계의 소프트웨어 보간기 개발)

  • Yang, Min-Yang;Hong, Won-Pyo
    • Journal of the Korean Society for Precision Engineering
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    • v.13 no.12
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    • pp.99-105
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    • 1996
  • Increasing demands on precision machining of free-form surfaces have necessitated the tool to move not only with position error as small as possible, but also with smoothly varying feedrates. In this paper, linear, circular and spline interpolators were developed in reference-pulse type using PC. M-SAM and M-DAM were designed by the comparison and analysis of previous interpolation methods. Spline interpolator was designed to follow the free-form curves. To apply to the real cutting process, constant feedrate compensation and acceleration-deceleration compensation were conceived. Finally, its performance was tested using retrofitted milling machine. As a result, new interpolation algorithm is favorable in precision machining of free-form curves.

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Development of Onboard Orbit Generation Algorithm for GEO Satellite (정지궤도 위성의 탑재 궤도 생성 알고리듬 개발)

  • Yim, Jo Ryeong;Park, Bong-Kyu;Park, Young-Woong;Choi, Hong-Taek
    • Aerospace Engineering and Technology
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    • v.13 no.2
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    • pp.7-17
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    • 2014
  • This technical paper deals with development of on-board orbit generation algorithm for GEO Satellite. This paper presents the research analysis results performed in order to improve the accuracy of the existing algorithm used for generating real-time orbit information for GEO satellite. The error impact on orbit accuracy due to the orbit error sources were analyzed with the algorithm suggested by this research. As a result of the analyses, it is found that the initial orbit should be determined with an accuracy of less than 50 m and the reference position angle error for the ground station and the satellite should be maintained within ${\pm}0.0025deg$ in order to meet the orbit accuracy specification. The development of on-board flight software based on the new algorithm was accomplished and the performance verification is ongoing by using a software based performance verification tool.