• Title/Summary/Keyword: 개루프제어

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Open-Loop Control of Combustion Instability in Hot-Firing Test Using Gaseous Hydrocarbon Fuel (기체 탄화수소 연료 연소시험에서 연소불안정의 개루프 제어)

  • Hwang, Donghyun;Ahn, Kyubok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.6
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    • pp.28-36
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    • 2018
  • A study was conducted to apply open-loop control to the combustion instability in a dump combustor using gaseous hydrocarbon fuels. Control power and frequency were varied by employing a loudspeaker under combustion conditions with similar characteristic chemistry times of the fuels. In the case of open-loop control where the frequency was identical to the combustion instability frequency, the open-loop control power affected the control performance. Results obtained from conducted open-loop control tests, where the frequency was different from the combustion instability frequency, show that setting the open-loop control frequency similar to the combustion instability frequency is effective.

Finite element analysis for dynamic behavior of a machine tool structure fed in open loop control (개루프제어로 이송되는 공작기계 구조물의 동적 거동을 위한 유한 요소 해석)

  • Choi, Jin-Woo;Lee, Tae-Hong
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.19 no.5
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    • pp.596-602
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    • 2010
  • In this study, a fmite element model was developed for analysis of feeding a structure in open loop control The finite element analysis (FEA) can simulate dynamic behavior of the structure of a machine tool rapidly traveling with a screw feeding driving system. The feeding mechanism was implemented with screw element of the FEA tool used in this study. The procedure was developed for the dynamic transient FEA. First, motion parameters such as jerk and velocity were introduced for the structure to be fed in open loop control When its traveling distance was determined, set-points for the distance were generated based on the motion parameters. The set-points were applied to the FE model constructed for the traveling structure. The FEA was executed and evaluated. In this study, the FEA procedure was applied to the column of a machine tool and the dynamic behavior of the column was evaluated. The FEA helps in evaluation of the motion characteristics of a structure. The convergence time of the structure vibration posterior to feeding termination can be estimated and the stiffness of the flexible structure is also evaluated against jerk, and acceleration. It provides the feeding force which is helpful in selection of the feeding motor.

Vibrational Control of an Underactuated Mechanical System : Control Design Using the Averaging Method (불충분한 작동기를 가진 기계시스템의 진동적제어: 평균화기법을 통한 제어 설계)

  • 이강렬;홍금식;이교일
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1995.10a
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    • pp.534-537
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    • 1995
  • An open loop vibrational control of underactuated mechanical system with amplitude and frequency modulations is investigated. The underactuated systems sonsidered in the paper are assumed to have free joints with no brake. The active joints are positioned first by a linearizing control, and then periodic oscillatory input are applied to them to move the remaining free joints to their desired states. A systematic way of obtaining averaged systems for the underactuated systems with oscillatory vibration is developed. A complete solution to the open loop control strateegy in terms of determining amplitudes and frequencies for general system is still under investigation. However, a specific control design for 2R manipulator which is obtained through the averaged system is demonstrated.

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Small signal analysis of LLC resonant converter for high switching frequency (고주파 LLC 공진형 컨버터의 소신호 분석과 제어기 설계)

  • Park, Hwapyeong;Lee, SangJung;Jung, Jeehoon
    • Proceedings of the KIPE Conference
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    • 2015.07a
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    • pp.405-406
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    • 2015
  • 높은 동작 주파수를 가지는 LLC 공진형 컨버터는 수동 소자들의 사이즈가 작아져 전력밀도가 증가하는 장점이 있다. 하지만 높은 전력 밀도를 구현하기 위한 작은 수동 소자들은 컨버터 개루프 이득을 변동시키고 기존의 피드백 제어기를 사용할 경우 불안정한 동작을 가진다. 따라서 적절한 위상 및 이득 여유을 가지는 루프 이득을 구현하기 위하여 작은 수동 소자 사용에 따른 개루프 이득을 분석하여 적절한 피드백 제어기를 설계한다. 본 논문은 500 kHz의 동작 주파수를 가지는 LLC 공진형 컨버터를 설계 및 제작하고 수동 소자의 크기에 따른 소신호를 분석한다. 이를 바탕으로 적절한 제어기를 설계하고 안정한 동작을 검증하였다.

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A Suppression of Residual Vibration on the Flexible Structures by Input Shaping (입력설계기법에 의한 유연구조물의 잔류진동제어)

  • Park, Myoungho;Han, Myoungseok;Park, Sungjong
    • 대한공업교육학회지
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    • v.31 no.2
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    • pp.364-380
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    • 2006
  • This paper presents a procedure for designing command to maneuver flexible structure with very little residual vibration, even in the presence of modeling errors. For the open loop maneuver, the various shaped profiles using multiple step inputs delayed in time are considered for robustness and compared with the responses of rigid body and flexible body in virtue of simulations and experiments. Input shaping generates vibration-reducing shaped commands through convolution of an impulse sequence with the desired command. A flexible model with a cylindrical hub and four symmetric appendages is considered to examine the responses to real plant, and to illustrate the effectiveness of the proposed shapers. The appendages are long and flexible, leading to low frequency vibration under any control action. It is shown by a series of simulation that a properly designed feedback controller with input shaper performs well, as compared with open loop controller with input shaper. The control objective is to achieve a fast settling time of residual vibration to flexible structure and robustness (insensitivity)to plant uncertainty, to eliminate residual vibration.

A study on the control law of Automatic Rudder Trim System for turbo prop aircraft (터보 프롭 항공기 자동러더트림장치 제어법칙에 관한 연구)

  • 박완기;이광현;김병수
    • Journal of the Korea Institute of Military Science and Technology
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    • v.2 no.1
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    • pp.121-131
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    • 1999
  • Automatic Rudder Trim System(ARTS) is a device to reduce the pilot's work load for rudder trimming greatly required in varying abruptly aircraft's engine power. This paper represents a technical analysis and a design of control law of the ARTS. The control law of the ARTS is designed based on the analysis of aircraft's characteristics, system's requirements, and limitations. The control law is comprised of open loop control using the rudder trim map for a specific aircraft and closed loop control to compensate the error of the open loop control system. flight test results show that the ARTS can reduce pilot's work load for rudder trimming dramatically and can compensate the aircraft's transient yaw motion.

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Design and Fabrication of Wide Electrical Tuning Range DRO Using Open-Loop Method (개루프 방법에 의한 확장된 전기적주파수조정범위를 갖는 유전체공진기발진기의 설계 및 제작)

  • Jeong, Hae-Chang;Oh, Hyun-Seok;Yang, Seong-Sik;Yeom, Kyung-Whan
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.20 no.6
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    • pp.570-579
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    • 2009
  • In this paper, we presented a Vt-DRO with a wide electrical frequency tuning range, using open-loop gain method. The Vt-DRO was composed of 3-stages, resonator, amplifier and phase shifter. In order to satisfy an oscillation condition, we determined magnitude and phase of each stage. The measured S-parameter of cascaded 3-stages shows open-loop oscillation condition. Also, using measured open loop group delay, we derived the relation for electrical frequency tuning range. The Vt-DRO was implemented by connecting the input and the output of the designed open-loop and resulted in closed-loop. As a results, tuning-range of Vt-DRO is 82 MHz, which is close to the predicted results for tuning voltage 0${\sim}$10 V and shows linear frequency tuning at the center frequency of 5.3 GHz. The phase noise is -104 ${\pm}$1 dBc/Hz at 100 kHz offset frequency and power is 5.86${\pm}$1 dBm respectively.

Friction and It's Nonlinear Compensation for Rotor Position Control (회전축계 위치제어에 대한 마찰과 비선형 보상)

  • 장용훈;최연선
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1990.10a
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    • pp.157-162
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    • 1990
  • 기계의 정밀도 향상을 위하여는 기계에 대한 보다 정확한 해석을 요구한다. 그러나 실제 기계 시스템은 마찰, Backlash, Saturation등과 같은 비서형 특 성을 가지고 있어 시스템의 해석 및 제어가 어렵게 된다. 특히, 축, 링크, 기 어, 풀리, 베어링등의 기계요소에서는 마찰로 인해 정밀도가 크게 덜어지고 있어, 마찰에 의한 동특성 및 제어는 많은 연구자들에 의해 관심의 대상이 되어 왔다. 마찰력을 고려한 기계시스템의 운동은 정지상태 근처에서 마찰력 의 변화가 심한 비선형 동특성을 보이고 있어 그 해석에 어려움을 겪고 있 다. 실제 마찰이 저속에서 고급 비선형임에도 불구하고 가장 널리 사용되는 형태의 모델로서 쿨통 마찰을 고려한 운동방정식 조차 비선형성으로 인하여 해석에 어려움이 따르고 있다. 마찰은 오랜동안 연구되어 오면서 Fig.1, Fig2 와 같이 등가선형점성 감쇠, 쿨통마찰, 정적마찰로 모델화되거나 이들의 조 합으로 나타내었다[1-5]. 마찰력은 시간영역에서도 연구되어 Walrath[7]는 Fig.3-a의 속도가 역전되는 지점에서 마찰토오크가 .+-.Tf를 공유하는 문제 를 고려하기 위해, Fig.3-b와 같이 동적마찰모델을 사용하였다. 최근의 연구 로서 Armstrong[7]은 마찰의 위치의존성을 고려한 정확한 마찰모델을 설정 하여 개루프제어에 적용, 좋은 제어특성을 확인하였고, Canudas[8]는 저속영 역에서 overcompensation시 limit cycle과 gain의 관계를 해석하였다.

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The Characteristics of Open-loop Trajectory and Time-to-go Estimation for Impact Angle Control Optimal Guidance through Inverse Optimal Problem (역최적 문제를 통한 충돌각 제어 최적유도법칙의 개루프 비행궤적 특성 및 Time-to-go 예측)

  • Lee, Yong-In;Lee, Jin-Ik
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.3
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    • pp.5-12
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    • 2008
  • This paper presents the features of an impact angle constrained open-loop optimal trajectory which is given by a function of initial conditions and optimal guidance gains. Using missile motion described by linearized kinematic equations and a proper form of performance index, an inverse optimal problem is suggested to investigate the gains related to the performance index. The flight trajectory and time-to-go can be shaped in terms of the optimal guidance gains. The results are evaluated by 3-DOF simulation.

Analysis of Torque Characteristics And Modeling of 4Phase And 5Phase Hybrid Type Step Motors (4상과 5상 하이브리드형 스텝모터의 모델링 및 토크특성해석)

  • Choi, D.S.;Baek, S.H.;Kim, Y.;Yun, S.Y.;Chung, I.R.;Chang, H.S.
    • Proceedings of the KIEE Conference
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    • 1998.07a
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    • pp.205-208
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    • 1998
  • 영구자석형 하이브리드 스텝모터는 저가이며 개루프 제어 장치와 더불어 기계적인 제어시스템분야에서 광범위하게 이용되어 왔다. 서보모터 기술의 발달에 따라 영구자석형 스템모터는 고토크, 정밀제어의 응용분야에 있어 중요한 위치를 계속 점유하고 있다. 스텝모터는 외란으로서 작용하는 부하의 영향에 대해 안정한 견고성을 가지며, 적당한 속도와 양호한 분해능의 조합으로 신뢰도가 높고, 구조상 단순한 특징을 갖고 있다. 최근 저가의 개루프 위치제어 장치에 2상 스텝모터와 5상 스텝모터 중에서 어느 것이 더 적합한가에 대한 기술적인 주제가 주목할 어느 것이 더 적합한가에 대한 기술적인 주제가 주목할 만한 문제로 대두되고 있다. 이 두 기기의 구조는 거의 유사하며 같은 원리로 동작한다. 본 논문에서는 이 두 기기의 동작이 명백히 비교될 수 있는 기본적인 수준으로 돌아가서 두 모델을 고찰했다.

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