• Title/Summary/Keyword: Tuning Effect

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Dynamic Modeling of the Stator Core of the Electrical Machine Using Anisotropic Characteristics (이방성을 고려한 회전기기 고정자 코어의 동적 모델링)

  • Kim, Heui-Won;Lee, Soo-Mok;Kim, Kwan-Young
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11a
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    • pp.401.1-401
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    • 2002
  • The state core of a motor/generator was modeled using dynamic model updating technique based on the modal testing work. In order to take into account the orthotropic effect of laminated structure the axial, radial and circumferential properties of the solid element were separately varied to match the primary modes of the stator core which were extracted from the modal testing. Comparison of the results after model tuning showed fairly good coincidence with measured data.

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Quaternary InGaAsP MQW QCSE Tuned Multichannel Source for DWDM Networks (고밀도 파장분할다중 네트워크 응용을 위한 Quaternary InGaAsP 다중양자우물 QCSE 다중 채널원)

  • Song, Ju-Bin
    • Journal of the Institute of Electronics Engineers of Korea SD
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    • v.41 no.4
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    • pp.49-55
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    • 2004
  • This paper describes a 1550 nm multichannel source using Quatemary/quatemary multiple quantum well (MQW) InGaAsP/InGaAsP quantum confined Stark effect (QCSE) tuning for dense wavelength division multiplex (DWDM) systems with 140 ㎓ channel spacing and 32 nm channel selection bandwidth.

Integrated Guidance and Control Design Based on Adaptive Neural Network for Unpowered Air Vehicle (무추력 비행체를 대상으로 한 적응 통합 유도제어기 설계)

  • Kim, Boo-Min;Sung, Duck-Yong;Sung, Jea-Min;Kim, Byoung-Soo
    • Journal of Institute of Control, Robotics and Systems
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    • v.15 no.1
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    • pp.15-22
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    • 2009
  • The guidance controller of the conventional aircraft consists of inner-loop (autopilot) and outer-loop (guidance). If the guidance controller can be designed as an integrated guidance and control (IGC), the various advantages exist. The integrated guidance and control formulation can compensate for the effect of autopilot lag. An integrated approach also helps avoid the iterative procedure involved in tuning the guidance and autopilot subsystems, if designed separately. Integrated design is also less susceptible to saturation and stability problems. This paper presents an approach to IGC design for the unpowered air vehicle with the only flaperon using a combination of adaptive output feedback inversion and backstepping techniques. Adaptive neural networks are trained online with available measurements to compensate for unmodeled nonlinearities in the design process.

The effect of strain on the electronic properties of MoS2 monolayers

  • Park, Soon-Dong;Kim, Sung Youb
    • Coupled systems mechanics
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    • v.5 no.4
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    • pp.305-314
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    • 2016
  • We utilize first-principles calculations within density-functional theory to investigate the possibility of strain engineering in the tuning of the band structure of two-dimensional $MoS_2$. We find that the band structure of $MoS_2$ monolayers transits from direct to indirect when mechanical strain is applied. In addition, we discuss the change in the band gap energy and the critical stains for the direct-to-indirect transition under various strains such as uniaxial, biaxial, and pure shear. Biaxial strain causes a larger change, and the pure shear stain causes a small change in the electronic band structure of the $MoS_2$ monolayer. We observe that the change in the interaction between molecular orbitals due to the mechanical strain alters the band gap type and energy.

DEVELOPMENT OF WIDEBAND TUNABLE E-BAND(60-70 GHz) GUNN OSCILLATOR (광대역 특성을 갖는 E-band(60-70 GHz) Gunn 발진기 제작)

  • 김현주;한석태;김태성;김용기
    • Journal of Astronomy and Space Sciences
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    • v.17 no.2
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    • pp.221-232
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    • 2000
  • A Gunn waveguide-oscillator, mechanically tunable from 60 to 70 GHz, has been developed for use as a local oscillator(LO) is millimeter radio telescope. Disc size, post size and characteristics of Gunn diode have an effect on the frequency tuning characteristics of Gunn oscillator. In this paper we report experimental results and design criteria for a wideband tunable Gunn oscillator. The developed Gunn oscillator has been used in the 100/150 GHz band dual channel receiver for the Taeduk Radio Astronomy Observatory.

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A Study on the Fabrication and Analysis of Mechanical Parts of a Dynamically Tuned Gyroscope (동조자이로스코우프 기계부의 제작 및 해석에 관한 연구)

  • 안창기;윤종욱;이장무
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1994.10a
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    • pp.930-937
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    • 1994
  • Straodown intertial navigation system(SDINS) is a navigational instrument necessary to guide and control a free vehicle. Dynamically Tuned Gyroscope(DTG) which is widely applied to SDINS convers a wide dynamic range and is simple and small. In study, the analysis of mechanical parts or sensor parts and research of balancing is performed for manufacturing a DTG. In error analysis the criterion considered during designing and manufacturing is established by quantitatively anayzing the effect of DTG performance by tolerance. And the theory of dynamic balancing is derived and unbalance is reduced through experiment. And the stiffness of flexure is verified by tuning experiment.

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Implementation of Remote Feedback Control System via Profibus-DP Network (Profibus-DP에서의 원격 피드백 제어 시스템 구축)

  • Lee, Kyung-Chang;Kang, Song;Lee, Suk
    • Journal of the Korean Society for Precision Engineering
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    • v.18 no.5
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    • pp.120-129
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    • 2001
  • As many sensors and actuators are used in many automated systems, various industrial networks are adopted for real-time distributed control. In order to take advantages of the networking, however, the network implementation should be carefully designed to satisfy real-time requirements considering network delays. This paper presents the implementation of a remote feedback control system via Profibus-DP net work for real-time distributed control More specifically, the effect of the network delay on the control performance evaluated on Profibus-DP testbed. Also, the traditional PID gain tuning methods are used to demonstrate the feasibility of the remote feedback control.

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A study on the performance prediction of 4 cycle 4 cylinder S.I. engine considering the unsteady flow in the intake and exhaust pipes (흡배기 관내의 비정상 유동을 고려한 4사이클, 4기통 전기.점화 기관의 성능 예측에 관한 연구)

  • 박성서;김응서
    • Journal of the korean Society of Automotive Engineers
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    • v.13 no.6
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    • pp.72-81
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    • 1991
  • In this study, the analytic investigation of the unsteady flow in the intake and exhaust pipes has been carried out using the method of characteristics in one direction to predict volumetric efficiency. Based on the calculated volumetric efficiency, three zone predictive analysis using Wiebe function was applied to predict the engine performance and the results were compared with experiment. Mixture in the cylinder is subdivided into three zones during combustion process in this analysis; adiabatic core zone, thermal boundary layer zone and unburned zone. In each zone, pressure, temperature and gas composition have been calculated. In conclusion, it is possible to take account of the intake and exhaust pipe tuning effect in predicting the engine performance, by the analytic solution of the unsteady flow in the pipes, and comparison of prediction with experimental results shows a good agreement on the pressure variation in the intake and exhaust pipes which has a direct influence on the volumetric efficiency and performance of the engine.

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Improvement of aeroelastic stability of hingeless helicopter rotor blade by passive piezoelectric damping

  • Yun, Chul-Yong;Kim, Seung-Jo
    • International Journal of Aeronautical and Space Sciences
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    • v.7 no.1
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    • pp.54-64
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    • 2006
  • To augment weakly damped lag mode stability of a hingeless helicopter rotor blade in hover, piezoelectric shunt with a resistor and an inductor circuits for passive damping has been studied. A shunted piezoceramics bonded to a flexure of rotor blade converts mechanical strain energy to electrical charge energy which is dissipated through the resistor in the R-L series shunt circuit. Because the fundamental lag mode frequency of a soft-in-plane hingeless helicopter rotor blade is generally about 0.7/rev, the design frequency of the blade system with flexure sets to be so. Experimentally, the measured lag mode frequency is 0.7227/rev under the short circuit condition. Therefore the suppression mode of this passive damping vibration absorber is adjusted to 0.7227/rev. As a result of damping enhancement using passive control, the passive damper which consists of a piezoelectric material and shunt circuits has a stabilizing effect on inherently weakly damped lag mode of the rotor blades, at the optimum tuning and resistor condition.

Design of Nonlinear PID Controller Based on Immune Feedback Mechanism (면역 피드백 메카니즘에 기초한 비선형 PID 제어기 설계)

  • Park Jin-Hyun;Choi Young-Kiu
    • The Transactions of the Korean Institute of Electrical Engineers D
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    • v.52 no.3
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    • pp.134-141
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    • 2003
  • PID controllers with constant gains have been widely used in various control systems due to its powerful performance and easy implementation. But it is difficult to have uniformly good control performance in all operating conditions. In this paper, we propose a nonlinear variable PR controller with immune feedback mechanism. An immune feedback mechanism is based on the functioning of biological T-cells, they include both an active term, which controls response speed. and an inhibitive term, which controls stabilization effect. Therefore, the proposed nonlinear PID controller is based on immune responses of biological. immune feedback mechanism which is the cell mediated immunity and In order to choose the optimal nonlinear PID controller games, we also propose the tuning algorithm of nonlinear function parameter in immune feedback mechanism. To verify performance of the proposed algorithm, the speed control of nonlinear DC motor are performed. Front the simulation results, we have found that the proposed algorithm is more superior to the conventional constant fain PID controller.