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Advanced Load Follow Operation Mode for Korean Standardized Nuclear Power Plants (한국 표준 원전의 부하추종을 위한 운전 기법)

  • Park, Jung-In;Oh, Soo-Youl;Song, In-Ho;Hah, Yung-Joon;Kuh, Jung-Eui;Lee, Un-Chul
    • Nuclear Engineering and Technology
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    • v.24 no.2
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    • pp.183-192
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    • 1992
  • An advanced load-follow operation mode, Mode K, is presented for the Korean Standardized Nuclear Power Plants. The Mode K utilizes a heavy worth bank dedicated to axial shape control independent of the existing regulating banks. In Mode K, the heavy bank provides a wide range of axial shape control and a monotonic relationship between its motion and the axial shape change, which makes it easy to automate axial shape control. The achievement of full automatic reactor power control both for the reactivity and power shape would reduce the burden due to load-follow operation on the operator. Also, it can accommodate the frequen-cy control, which requires the plant to respond to the unexpected demand. The Mode K design concepts were tested using simulation responses of Yonggwang Units 3&4, the reference plants for the Korean Standardized Nuclear Power Plants. The results illustrate that the Mode K is an adequate operation mode to provide practical load-follow capabilities for the Korean Standardized Nuclear Power Plants.

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On-Chip Full CMOS Current and Voltage References for High-Speed Mixed-Mode Circuits (고속 혼성모드 집적회로를 위한 온-칩 CMOS 전류 및 전압 레퍼런스 회로)

  • Cho, Young-Jae;Bae, Hyun-Hee;Jee, Yong;Lee, Seung-Hoon
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.40 no.3
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    • pp.135-144
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    • 2003
  • This work proposes on-chip full CMOS current and voltage references for high-speed mixed-mode circuits. The proposed current reference circuit uses a digital-domain calibration method instead of a conventional analog calibration to obtain accurate current values. The proposed voltage reference employs internal reference voltage drivers to minimize the high-frequency noise from the output stages of high-speed mixed-mode circuits. The reference voltage drivers adopt low power op amps and small- sized on-chip capacitors for low power consumption and small chip area. The proposed references are designed, laid out, and fabricated in a 0.18 um n-well CMOS process and the active chip area is 250 um x 200 um. The measured results show the reference circuits have the power supply variation of 2.59 %/V and the temperature coefficient of 48 ppm/$^{\circ}C$ E.

Design of a High Performance Multiplier Using Current-Mode CMOS Quaternary Logic Circuits (전류모드 CMOS 4치 논리회로를 이용한 고성능 곱셈기 설계)

  • Kim, Jong-Soo;Kim, Jeong-Beom
    • Journal of IKEEE
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    • v.9 no.1 s.16
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    • pp.1-6
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    • 2005
  • This paper proposes a high performance multiplier using CMOS multiple-valued logic circuits. The multiplier based on the Modified Baugh-Wooley algorithm is designed with current-mode CMOS quaternary logic circuits. The multiplier is functionally partitioned into the following major sections: partial product generator block(binary-quaternary logic conversion block), current-mode quaternary logic full-adder block, and quaternary-binary logic conversion block. The proposed multiplier has 4.5ns of propagation delay and 6.1mW of power consumption. This multiplier can easily adapted to the binary system by the encoder and the decoder. This circuit is designed with 0.35um standard CMOS process at 3.3V supply voltage and 5uA unit current. The validity and effectiveness are verified through the HSPICE simulation.

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Power Allocation and Mode Selection in Unmanned Aerial Vehicle Relay Based Wireless Networks

  • Zeng, Qian;Huangfu, Wei;Liu, Tong
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • v.13 no.2
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    • pp.711-732
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    • 2019
  • Many unmanned aerial vehicle (UAV) applications have been employed for performing data collection in facilitating tasks such as surveillance and monitoring objectives in remote and dangerous environments. In light of the fact that most of the existing UAV relaying applications operate in conventional half-duplex (HD) mode, a full-duplex (FD) based UAV relay aided wireless network is investigated, in which the UAV relay helps forwarding information from the source (S) node to the destination (D). Since the activated UAV relays are always floating and flying in the air, its channel state information (CSI) as well as channel capacity is a time-variant parameter. Considering decode-and-forward (DF) relaying protocol in UAV relays, the cooperative relaying channel capacity is constrained by the relatively weaker one (i.e. in terms of signal-to-noise ratio (SNR) or signal-to-interference-plus-noise ratio (SINR)) between S-to-relay and relay-to-D links. The channel capacity can be optimized by adaptively optimizing the transmit power of S and/or UAV relay. Furthermore, a hybrid HD/FD mode is enabled in the proposed UAV relays for adaptively optimizing the channel utilization subject to the instantaneous CSI and/or remaining self-interference (SI) levels. Numerical results show that the channel capacity of the proposed UAV relay aided wireless networks can be maximized by adaptively responding to the influence of various real-time factors.

Full structure pseudo-dynamic test method and application based on OpenSees-OpenFresco-MTS

  • Zhen Tian;Yuan Cheng;Xuechong Ren;Mengmeng Yang
    • Structural Monitoring and Maintenance
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    • v.11 no.3
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    • pp.173-185
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    • 2024
  • Currently, the electro-hydraulic servo loading control system manufactured by MTS, OpenFresco hybrid test interface software and OpenSees finite element software are widely used in structure laboratories to carry out hybrid test, but there is no relevant public information about full structure pseudo-dynamic test based on the above software and hardware. In order to study the feasibility of using the above software and hardware to carry out full structure pseudo-dynamic test, the full structure pseudo-dynamic virtual experiments of a single degree of freedom (SDOF) structure and a two degrees of freedom (2DOFs) structure are carried out based on the MTS 793 Demo Mode, and the results are respectively compared with the finite element analysis method. The results show that the finite element analysis results and full structure pseudo-dynamic virtual experiment results are highly consistent, which verifies the feasibility of carrying out the full structure pseudo-dynamic test based on the above software and hardware. Then, a three story steel frame full structure pseudo-dynamic test is conducted, and the smooth implementation of full structure pseudo-dynamic test of the three story steel frame further verifies the reliability of thistesting method. The implementation method of carrying out the full structure pseudo-dynamic tests are introduced in detail, which can provide some reference for relevant research.

Control Law Design for a Tilt-rotor Unmanned Aerial Vehicle with a Nacelle Mounted WE (Wing Extension) (체공성능 향상을 위한 확장날개 틸트로터 무인기의 제어법칙설계)

  • Kang, Young-Shin;Park, Bum-Jin;Cho, Am;Yoo, Chang-Sun
    • Journal of Institute of Control, Robotics and Systems
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    • v.20 no.11
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    • pp.1103-1111
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    • 2014
  • The results of control law design for a tilt-rotor unmanned aerial vehicle that has a nacelle mounted wing extension (WE) are presented in this paper. It consists of a control surface mixer, stability and control augmentation system (SCAS), hold mode for altitude / speed / heading, and a guidance mode for preprogram and point navigation which includes automatic take-off and landing. The conversion corridor and the control moments derivatives between the original tilt-rotor and its variant of the nacelle mounted WE were compared to show the effectiveness of the WE. The nacelle conversion of the original tilt-rotor starts when the airspeed is greater than 30 km/h but its WE variant starts at 0 km/h in order to reduce the drag caused by the high incidence angle of the WE. The stability margins of the inner loop are presented with the optimization approach. The outer loops for the hold mode are designed with trial and error methods with linear and nonlinear simulation. The main control parameter for altitude control of the helicopter mode is thrust command and it is transferred to the pitch attitude command in airplane mode. Otherwise, the control parameter for the speed of the helicopter mode is the pitch attitude command and it is transferred to the thrust command in airplane mode. Therefore the speed and altitude hold mode are coupled to each other and are engaged at the same time when an internal pilot engages any of the altitude or speed hold modes. The nonlinear simulation results of the guidance control for the preprogrammed mode and point navigation are also presented including automatic take-off and landing in order to prove the full control law.

Design of Low-power Serial-to-Parallel and Parallel-to-Serial Converter using Current-cut method (전류 컷 기법을 적용한 저전력형 직병렬/병직렬 변환기 설계)

  • Park, Yong-Woon;Hwang, Sung-Ho;Cha, Jae-Sang;Yang, Chung-Mo;Kim, Sung-Kweon
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.34 no.10A
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    • pp.776-783
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    • 2009
  • Current-cut circuit is an effective method to obtain low power consumption in wireless communication systems as high speed OFDM. For the operation of current-mode FFT LSI with analog signal processing essentially requires current-mode serial-to-parallel/parallel-to-serial converter with multi input and output structure. However, the Hold-mode operation of current-mode serial-to-parallel/parallel-to-serial converter has unnecessary power consumption. We propose a novel current-mode serial-to-parallel/parallel-to-serial converter with current-cut circuit and full chip simulation results agree with experimental data of low power consumption. The proposed current-mode serial-to-parallel/parallel-to-serial converter promise the wide application of the current-mode analog signal processing in the field of low power wireless communication LSI.

Novel Compact Bandpass Filter Based on Folded Half Mode Substrate Integrated Waveguide Cavities

  • Gong, Ke;Hong, Wei;Chen, Jixin;Tang, Hongjun;Hou, Debin;Zhang, Yan
    • Journal of electromagnetic engineering and science
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    • v.10 no.3
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    • pp.179-182
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    • 2010
  • This paper proposed a novel compact bandpass filter with folded half mode substrate integrated waveguide (FHMSIW) cavities using two-layer printed circuit board(PCB) process. The area of the FHMSIW filter is reduced by nearly 50 % and 75 % compared with half mode substrate integrated waveguide(HMSIW) filter and substrate integrated waveguide(SIW) filter, respectively. A four-pole Chebyshev FHMSIW bandpass filter at C-band has been designed, simulated and fabricated. Measured results are presented and found to agree with the full-wave simulated results by using Ansoft HFSS. The filter shows good performance and compact size.

Periodic-Cell Simulations for the Microscopic Damage and Strength Properties of Discontinuous Carbon Fiber-Reinforced Plastic Composites

  • Nishikawa, M.;Okabe, T.;Takeda, N.
    • Advanced Composite Materials
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    • v.18 no.1
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    • pp.77-93
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    • 2009
  • This paper investigated the damage transition mechanism between the fiber-breaking mode and the fiber-avoiding crack mode when the fiber-length is reduced in the unidirectional discontinuous carbon fiber-reinforced-plastics (CFRP) composites. The critical fiber-length for the transition is a key parameter for the manufacturing of flexible and high-strength CFRP composites with thermoset resin, because below this limit, we cannot take full advantage of the superior strength properties of fibers. For this discussion, we presented a numerical model for the microscopic damage and fracture of unidirectional discontinuous fiber-reinforced plastics. The model addressed the microscopic damage generated in these composites; the matrix crack with continuum damage mechanics model and the fiber breakage with the Weibull model for fiber strengths. With this numerical model, the damage transition behavior was discussed when the fiber length was varied. The comparison revealed that the length of discontinuous fibers in composites influences the formation and growth of the cluster of fiber-end damage, which causes the damage mode transition. Since the composite strength is significantly reduced below the critical fiber-length for the transition to fiber-avoiding crack mode, we should understand the damage mode transition appropriately with the analysis on the cluster growth of fiber-end damage.

EMI Noise Reduction with New Active Zero State PWM for Integrated Dynamic Brake Systems

  • Baik, Jae-Hyuk;Yun, Sang-Won;Kim, Dong-Sik;Kwon, Chun-Ki;Yoo, Ji-Yoon
    • Journal of Power Electronics
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    • v.18 no.3
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    • pp.923-930
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    • 2018
  • Based on the application of an integrated dynamic brake (IDB) system that uses a PWM inverter fed-AC motor drive to operate the piston, a new active zero state PWM (AZSPWM) is proposed to improve the stability and reliability of the IDB system by suppressing the conducted electro-magnetic interference (EMI) noise under a wide range of load torque. The new AZSPWM reduces common-mode voltage (CMV) by one-third when compared to that of the conventional space vector PWM (CSVPWM). Although this method slightly increases the output current ripple by reducing the CMV, like the CSVPWM, it can be used within the full range of the load torque. Further, unlike other reduced common-mode voltage (RCMV) PWMs, it does not increase the switching power loss. A theoretical analysis is presented and experiments are performed to demonstrate the effectiveness of this method.