• Title/Summary/Keyword: Airplane

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A study on the Application Technique to Remote Sensing Image for Optimum Route Selection of the Two-Tract Line Railroad (복선철도의 최적노선 선정을 위한 원격탐사영상의 적용실험연구)

  • 연상호;장상규;홍일화
    • Proceedings of the Korean Society of Surveying, Geodesy, Photogrammetry, and Cartography Conference
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    • 2004.04a
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    • pp.165-169
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    • 2004
  • Recently remote sensing technology is applied for construction projects planning and design areas by use of high resolution satellite images according to engineering application technology in the various experimental tasks. In this study, It was applied for optimum route selection methods and basic design by comparing to present railway and new expand dual railway route on the new construction plan path of 20km at national railway lines, and then showed 3-dimensional images and fly simulation images to possibility for various application as low cost and short time compare to airplane and helicopters survey methods. As a results of its applied, It gained the results not only improvement of present methods but also real various application possibilities.

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A Study for the System Light-Weighting Technology of Urban Railway Vehicle (도시철도차량의 시스템 경량화 기술에 관한 연구)

  • Park, Kwang-Bok;Jung, Hyun-Seung;Kim, Jong-Woon
    • Proceedings of the KSR Conference
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    • 2011.10a
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    • pp.2965-2972
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    • 2011
  • The 21th century is carried out a rearing activity of green industries as a part of friendly echo policy for preservation of earth environment. Korean government is spreaded on a whole country to setting up a goal to a sustainable growth power of national for low carbon green growth. The recently rolling stock is received the footlights as a best friendly echo transportation of transport system of automobile, airplane, ship etc., also that is playing a big role to reduction of $CO_2$ greenhouse gas and a discharge of air pollution. This study was carried out the investigation and analysis for technology trend of the system light-weighting of a recently urban railway vehicle on commercial operating in domestic and foreign countries. As the results are proposed a short-term development technology and a long-term development technology of the system light-weighting to be developed for reduction weight of urban railway vehicle.

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Development of Image Analysis Program for Microstructure in Semi-solid Forming Product (반용융 성형 제품의 미세조직 영상분석을 위한 프로그램 개발)

  • Kwon, Soon-Goo;Park, Joon-Hong
    • Journal of the Korean Society of Industry Convergence
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    • v.4 no.1
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    • pp.3-9
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    • 2001
  • Many products related to automobile and airplane have been manufactured by semi-solid process. There are many parameters in semi-solid process such as punch velocity, die temperature, and solid fraction of material. Among these parameters, solid fraction of material is one of the most important factors to determine quality of product. To obtain solid fraction of a certain semi-solid product is very necessary and useful for inspecting and analyzing the product. In this paper, image analysis program for microstructure by semi-solid forming process has been developed with the simple apparatus such as a personal computer and scanner, instead of expensive image analyzer.

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Automatic Landing in Adaptive Gain Scheduled PID Control Law

  • Ha, Cheol-Keun;Ahn, Sang-Won
    • 제어로봇시스템학회:학술대회논문집
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    • 2003.10a
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    • pp.2345-2348
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    • 2003
  • This paper deals with a problem of automatic landing guidance and control system design. The auto-landing control system for the longitudinal motion is designed in the classical PID controller. The controller gains are properly adapted to variation of the performance using fuzzy logic as a gain scheduler for the PID gains. This control logic is applied to the problem of the automatic landing control system design. From the numerical simulation using the 6DOF nonlinear model of the associated airplane, it is shown that the auto-landing maneuver is successfully achieved from the start of the flight conditions: 1500 ft altitude, 250 ft/sec airspeed and zero flight path angle.

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Design and Implementation of UAV's Autopilot Controller

  • Lee, Jeong-Hwan;Lee, Ki-Sung;Jeong, Tae-Won
    • 제어로봇시스템학회:학술대회논문집
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    • 2004.08a
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    • pp.52-56
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    • 2004
  • Unmanned Aerial Vehicles (UAVs) are remotely piloted or self-piloted aircraft by inputted program in advance or artificial intelligence. In this study Aileron and Elevator are used to control the movement of airplane for horizontal and vertical flights about its longitudinal and lateral axis. In an introduction, the drone was linearly modeled by extracting aerodynamic parameter through flight test and simulation, lift and drag coefficient corresponding to angle of attack, changes of pitching moment coefficient. In the main subject, the flight simulation was performed after constructing hardware using TMS320F2812 from TI company and PID with lateral and longitudinal controller for horizontal and vertical flights. Flying characteristics of two system were estimated and compared through real flight test with hardware equipped algorithm and adaptive algorithm that was applied to consider external factors such as turbulence. In conclusion the control performance of the controller with proposed algorithm was streamlined at lateral and longitudinal controller respectively, we will discuss guidance command to pass way point.

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A study on the VHDL Implementation of a RS coder for a FTS transceiver

  • Kim Woo Shik;Lim Jun Seok;Yoon Steve
    • Proceedings of the IEEK Conference
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    • 2004.08c
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    • pp.463-467
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    • 2004
  • A FTS (Flight Termination System) is a system that resides in a flying object such as a rocket, unmanned airplane, helicopter, missile, etc., receives commands from ground stations or detects coordinates automatically, and accomplishes a destruction command in case the object does not follow the presumed orbit. In this paper, we address the implementation of a communication modem for the FTS modem. We present general theory, simulation results using Matlab, and several results on the implementation using VHDL.

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STUDY OF ICING ACCRETION ON THE 2D AIRFOIL (2차원 에어포일에서의 결빙부착 수치해석)

  • Shin, H.B.;Choi, W.;Seo, S.J.;Ryu, J.B.
    • 한국전산유체공학회:학술대회논문집
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    • 2009.04a
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    • pp.21-26
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    • 2009
  • Ice accretion is one of the potential hazards in airplane flight, adversely affecting aircraft aerodynamic. There are two distinct icing analysis that can be simulated. One is predicting the effect of ice on the aerodynamic performance of airfoils when ice geometry is known. The other is simulating ice accretion. This work presents the method of icing accretion analysis. This work presents an Eulerian approach to calculate the droplet collection efficiency on the 2D airfoil. The initial flow solution are obtained the FLUENT and copled with droplet motion in the ambient condition.

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ISAR Imaging of Airplane-like Targets by Matrix Pencil Method (Matrix Pencil 방법에 의한 비행기 모형의 ISAR 영상화)

  • 유지희;권경일;이용희
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.12 no.2
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    • pp.299-307
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    • 2001
  • This paper presents a experimental study of Inverse Synthetic Aperture Radar(ISAR) imaging using Matrix Pencil(MP) method. A series of measurement for two types of target model was done in a Compact Range(CR)facility. The first target is a set of distributed slim cylinders to get a ISAR image of point-like scatterers. The second is UAV model representing a complex real target. The results show that ISAR images by MP method are better than by conventional FFT method under the realistic measurement conditions.

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A study on INS/GPS implementation of loosely coupled method for localization of mobile robot. (이동로봇의 위치 추정을 위한 약결합 방식의 INS/GPS 구현에 관한 연구)

  • Park, Myung-Hoon;Hong, Seung-Hong
    • Proceedings of the KIEE Conference
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    • 2004.11c
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    • pp.493-495
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    • 2004
  • In this paper, shows a research in accordance with the design the implementation of the localization system for mobile robot using INS(Inertial Navigation System) and GPS(Global Positioning System). First, a Strapdown Inertial Navigation System : SDINS is designed and implemented for low speed walking robot, by modifying Inertial Navigation System which is widely used for rocket, airplane, ship and so on. In addition, thesis proposes the localization of robot with the method of loosely coupled method by using Kalman Filter with INS/GPS integrated system to utilize assumed position and steed data from GPS.

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Instantaneous Power Control of Permanent Magnet AC Motor (영구자석형 교류전동기의 순시전력제한)

  • Youn, K.S.;Lee, C.H.;Hwang, J.H.;Kwon, W.H.
    • Proceedings of the KIEE Conference
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    • 1996.07a
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    • pp.274-277
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    • 1996
  • Vector controlled PMAC(Permanent Magnet AC) motor, with rare-earth permanent magnet, are suitable for servo system demanding fast speed response. However, abrupt acceleration and deceleration control for fast response requires big instantaneous input power. So general PI control of PMAC motors can't be applied for limited power supply system like airplane or portable equipment because of input power fluctuation. Proposed technique to restrain instantaneous input power use variable power limit depends on airgap flux power. Stability check for proposed system is done.

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