• 제목/요약/키워드: Reverse Simulation

검색결과 387건 처리시간 0.021초

CDMA 방식의 저궤도 이동위성통신 시스템 GLOBALSTAR 역방향 링크의 비트오율 및 채널용량에 관한 연구 (Bit error probability and channel capacity in the return link of GLOBALSTAR-A CDMA LEO mobile satellite system)

  • 강형진;김동인
    • 한국통신학회논문지
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    • 제22권7호
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    • pp.1448-1458
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    • 1997
  • In this paper the reverse link of the GLOBALSTAR-the representative CDMA LEO satellite system and LEO mobile satellite channel are developed by the SPW software simulation tool. And the performance of the system is evaluated. GLOBALSTAR is designed to give cellular-type service to hand-held user terminals through a constellation of 48 LEO satellites in circular orbites with 1414 Km altitude. Since LEO mobile satellite system communicates with mobile unit, it is suffered from severe multipath fading and shadowing. The fast mobility of LEO satellites makes the channel condition time vering. So, the LEO mobile satellite channel is different from land mobile channels. In this unique LEO satellite channel, it is shown that the performance of the GLOBALSTAR reverse link is varied according to the elevational angle, but this variation is overcome by satellite path diversity.

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LES에 의한 관류홴의 전산유동해석 (Computational Flow Analysis of a Cross-Flow Fan by LES)

  • 김장권;오석형
    • 동력기계공학회지
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    • 제14권6호
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    • pp.20-28
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    • 2010
  • The computational flow analysis using LES technique was carried out to investigate the flow characteristics of a RAC chassis consisting of a rear-guider, a stabilizer and a cross-flow fan. The commercial SC/Tetra software was used in this analysis. In view of the results so far achieved, the distribution trends of static pressure and velocity vector of central region except the edges of a CFFan are similar regardless of the number of revolution, and an eccentric vortex exists around the bottom blade of a CFFan. Also, a reverse flow is found in the region between stabilizer and CFFan. Moreover, near the edges of a CFFan, an eccentric vortex is separated to two vortexes. Also these vortexes increase the velocity near a rear-guider, and guide the flow near a rear-guider into stabilizer inlet. Therefore, the reverse flow region is formed in the bottom of a CFFan.

A New Accurate Equation for Estimating the Baseline for the Reversal Peak of a Cyclic Voltammogram

  • Oh, Sung-Hoon;Chang, Byoung-Yong
    • Journal of Electrochemical Science and Technology
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    • 제7권4호
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    • pp.293-297
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    • 2016
  • Here we propose a new equation by which we can estimate the baseline for measuring the peak current of the reverse curve in a cyclic voltammogram. A similar equation already exists, but it is a linear algebraic equation that over-simplifies the voltammetric curve and may cause unpredictable errors when calculating the baseline. In our study, we find a quadratic algebraic equation that acceptably reflects the complexity included in a voltammetric curve. The equation is obtained from a laborious numerical analysis of cyclic voltammetry simulations using the finite element method, and not from the closed form of the mathematical equation. This equation is utilized to provide a virtual baseline current for the reverse peak current. We compare the results obtained using the old linear and new quadratic equations with the theoretical values in terms of errors to ascertain the degree to which accuracy is improved by the new equation. Finally, the equations are applied to practical cyclic voltammograms of ferricyanide in order to confirm the improved accuracy.

조향계 유압 시미댐퍼의 성능해석 프로그램 개발 (Development of Performance Analysis Program for a Hydraulic Shimmy Damper of Steering System)

  • 이재천;정용승;김진홍
    • 한국자동차공학회논문집
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    • 제12권1호
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    • pp.174-183
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    • 2004
  • A program to analyze the performance characteristics of a hydraulic shimmy damper for automotive steering system was developed in this study. Dimensionless mathematical equations of the dynamics of shimmy damper for forward and reverse fluid flows were derived respectively and incorporated into the Simulink models. The program was validated by comparing the results of simulation and experiments for various frequencies of upstream ripple pressures into the damper. Low-pass filter characteristics of the shimmy damper at reverse flow was demonstrated which means that the shimmy damper could alleviate the high speed ripple pressures induced by the unbalance oscillation of tire in vehicle driving. The parameter sensitivity analysis was also conducted to identify the dominant parameters for the damper performance.

CDMA 역방향 링크에서 OPEN LOOP 전력제어 알고리즘 분석 (Analysis of OPEN LOOP Power Control in CDMA Reverse Link)

  • 이철희;박종안
    • 한국통신학회논문지
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    • 제22권4호
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    • pp.804-811
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    • 1997
  • In the CDMA mobile communication system, reverse power control can be used to minimize the interference level for a good quality of the voice channel, and used to maxmize the system capacity. In this paper, we have analyed the environment of the K-parameter and the access procedure for the mobile station, and proposed a new algorithm for the access probe procedure of the station. K-parameter is determined according to the environment of the base station and access probe can adaptively control the power according to the position changes of the mobile station or the rapid and various state changes of the channel. Simulation results in the limited test environment show that it can increase the system capacity and decrease the power comsumption of the mobile station while maintaining the good and stable quality of the voice channel.

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Photogrammetry-based reverse engineering method for aircraft airfoils prediction

  • Ba Zuhair, Mohammed A.
    • Advances in aircraft and spacecraft science
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    • 제8권4호
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    • pp.331-344
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    • 2021
  • Airframe internal and external specifications are the product of intensive intellectual efforts and technological breakthroughs distinguishing each aircraft manufacturer. Therefore, geometrical information characterizing aircraft primary aerodynamic surfaces remain classified. When attempting to model real aircraft, many members of the aeronautical community depend on their personal expertise and generic design principles to bypass the confidentiality obstacles and sketch real aircraft airfoils, which therefore vary for the same aircraft due to the different designers' initial assumptions. This paper presents a photogrammetric shape prediction method for deriving geometrical properties of real aircraft airframe by utilizing their publicly accessible static and dynamic visual content. The method is based on extracting the visually distinguishable curves at the fairing regions between aerodynamic surfaces and fuselage. Two case studies on B-29 and B-737 are presented showing how to approximate the sectional coordinates of their wing inboard airfoils and proving the good agreement between the geometrical and aerodynamic properties of the replicated airfoils to their original versions. Therefore, the paper provides a systematic reverse engineering approach that will enhance aircraft conceptual design and flight performance optimization studies.

New Modeling of Switching Devices Considering Power Loss in Electromagnetic Transients Program Simulation

  • Kim, Seung-Tak;Park, Jung-Wook;Baek, Seung-Mook
    • Journal of Electrical Engineering and Technology
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    • 제11권3호
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    • pp.592-601
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    • 2016
  • This paper presents the modeling of insulated-gate bipolar transistor (IGBT) in electromagnetic transients program (EMTP) simulation for the reliable calculation of switching and conduction losses. The conventional approach considering the physical property of switching devices requires many attribute parameters and large computation efforts. In contrast, the proposed method uses the curve fitting and interpolation techniques based on typical switching waveforms and a user-defined component with variable resistances to capture the dynamic characteristics of IGBTs. Therefore, the simulation time can be efficiently reduced without losing the accuracy while avoiding the extremely small time step, which is required in simulation by the conventional method. The EMTP based simulation includes turn-on and turn-off transients of IGBT, saturation state, forward voltage of free-wheeling diode, and reverse recovery characteristics, etc. The effectiveness of proposed modeling for the EMTP simulation is verified by the comparison with experimental results obtained from practical implementation in hardware.

트랙터의 전후진 자동 변속을 위한 전자식 액추에이터의 위치 제어 시스템 개발 (Development of Electric Actuator Position Control System for Automatic Shuttle Shifting of Tractor)

  • 최창현;우미나;이대현;김용주;정진희
    • Journal of Biosystems Engineering
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    • 제35권4호
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    • pp.224-230
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    • 2010
  • The purpose of this study was to develop position control system of an electric actuator for automatic shuttle shifting of a tractor. The electric actuator was installed at the link of the forward-reverse gearshift of the tractor transmission, and controlled in the ranges of forward, neutral, and reverse positions. The position control system of the electric actuator was developed based on PID (Proportional Integral Derivative) controller and transfer function of the electric actuator. The coefficients of the PID controller were determined by Ziegler-Nichols (Z-N) method and optimized using simulation program. The prototype AMT (Automated Manual Transmission) test unit of the tractor was installed and used to evaluate the performance of the position control. The evaluation system for the control performance consisted of forward-reverse actuator, motor driver, and controller. The tests were conducted as the controlled positions of the actuator were changed from neutral position to forward, neutral, and reverse positions in sequence. The sequential tests were repeated 20 times. The operations of changing the gearshift were considered as the step response of the control system. Maximum overshoot, settling time, and steady-state error were analyzed. The results showed that performance of the position control system was reasonable and qualified. The maximum overshoots, the steady-state errors, and the settling times of the position control system were 10~20%, 1~5%, and 0.92~1.49 sec, respectively. The modifications of the electric actuator will be required to enhance the performance of position control during field operation.

소형 2차원 레이저 스캐너용 F-theta 렌즈 역설계 (Reverse Design of F-Theta Lens for Compact Laser Scanner)

  • 최해운
    • 대한기계학회논문집A
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    • 제41권3호
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    • pp.213-218
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    • 2017
  • 리모트 용접용 2D 스캐너 F-theta 렌즈의 역설계가 광선 추적기법을 사용하여서 수행이 되었다. 렌즈의 곡면 및 렌즈간 거리를 변수로 설정하고 초점거리를 Marginal Ray Height 로 설정하여, 상용 광선추적기법 프로그램을 사용하여 무한반복 최적화를 수행 하였다. 최종목표 값을 설정 후 Merit Function에 정의된 기준에 따라, 최종 초점거리와 초점의 크기를 최종 목표 값 가중치로 설정하였다. 최적화된 렌즈는 총 4매이며, 벤치마킹된 상용렌즈의 초점거리(185mm) 보다는 다소 근거리인 137mm로 최적화 되었지만, 초점의 크기는 레이저 입사각에 따라 RMS 기준 $1.3{\mu}m$, $6.2{\mu}m$ 그리고 $16.1{\mu}m$로 계산 되었으며, 이는 상용렌즈에 근접하는 성능을 구현한다. 입사각별 왜곡도를 중첩 하여서 비교 분석한 결과, 입사각 $0^{\circ}$$12.5^{\circ}$에서는 기존 렌즈와 거의 유사한 형태로 나타나는 것을 볼 수가 있어, 본 연구에서 제안된 역설계기법이 사용자 환경에 따라서 효과적으로 적용되어 최적설계가 이루어질 수 있을 것으로 기대가 된다.

The aerostatic response and stability performance of a wind turbine tower-blade coupled system considering blade shutdown position

  • Ke, S.T.;Xu, L.;Ge, Y.J.
    • Wind and Structures
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    • 제25권6호
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    • pp.507-535
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    • 2017
  • In the strong wind shutdown state, the blade position significantly affects the streaming behavior and stability performance of wind turbine towers. By selecting the 3M horizontal axis wind turbine independently developed by Nanjing University of Aeronautics and Astronautics as the research object, the CFD method was adopted to simulate the flow field of the tower-blade system at eight shutdown positions within a single rotation period of blades. The effectiveness of the simulation method was validated by comparing the simulation results with standard curves. In addition, the dynamic property, aerostatic response, buckling stability and ultimate bearing capacity of the wind turbine system at different shutdown positions were calculated by using the finite element method. On this basis, the influence regularity of blade shutdown position on the wind-induced response and stability performance of wind turbine systems was derived, with the most unfavorable working conditions of wind-induced buckling failure of this type of wind turbines concluded. The research results implied that within a rotation period of the wind turbine blade, when the blade completely overlaps the tower (Working condition 1), the aerodynamic performance of the system is the poorest while the aerostatic response is relatively small. Since the influence of the structure's geometrical nonlinearity on the system wind-induced response is small, the maximum displacement only has a discrepancy of 0.04. With the blade rotating clockwise, its wind-induced stability performance presents a variation tendency of first-increase-then-decrease. Under Working condition 3, the critical instability wind speed reaches its maximum value, while the critical instability wind speed under Working condition 6 is the smallest. At the same time, the coupling effect between tower and blade leads to a reverse effect which can significantly improve the ultimate bearing capacity of the system. With the reduction of the area of tower shielded by blades, this reverse effect becomes more obvious.