• Journal of the Institute of Convergence Signal Processing
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• v.3 no.4
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• pp.49-56
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• 2002

In this paper, a new controller using non-linear compensator for position control is presented, which we can satisfy the given specifications more easily than the existing one. We suggest an improved PDFE(Integral with Proportional-Derivative-plus-Feedforward) controller by which both phase margin and bandwidth are controlled simultaneously in the controller design problem. Replacing the feed forward term in the PDFF system with a CDIDF(Complex Dual Input Describing Function), the desired phase margin is obtained without diminishing the bandwidth of the closed loop system. The effectiveness of the proposed controller is confirmed through simulations and experiments. As The results of these, we know that it is possible to adjust overall specifications by varying parameters in the improved PDFF system.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2002.02a
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• pp.104-110
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• 2002

본 연구는 보행형 관리기의 손으로 전달되는 진동특성을 실험적으로 해석하고 평가하며 방진 방안을 제시할 목적으로 수행되었다. 관리기의 작업기 중에서 설문을 통해 사용 빈도가 높은 3개의 작업기(중경로터리, 중경제초기, 구굴기)를 선정하였고 각 작업기별 진동수준을 측정하였다. 진동 방지 방안에 대해서는 4개의 방진 장치(고무 패드, 방진 장갑, 핸들 방진 장치, 엔진 마운트)를 선정하여 각 방진 장치별 진동수준을 측정하였다. 방진 장치의 성능을 정확하게 비교하기 위해 진동의 측정은 진동수준이 가장 높은 구굴기에서 수행되었다. 실험결과에 의하면 관리기 작업이 작업자의 인체에 해를 끼칠 위험이 매우 크지만 이 결과는 작업자가 매일 3시간씩 관리기를 사용할 경우를 기준으로 설정한 값이기 때문에 실제로 관리기 사용일수가 많지 알은 대부분의 우리나라 사용자들에게 적용하는데는 한계가 있음을 밝힌다. 그렇다 하더라도 관리기의 주 사용자는 보행형 관리기 뿐만 아니라 보행형 경운기나 보행형 이앙기 등의 손으로 전달되는 진동이 심한 기계를 함께 사용하는 경우가 많음을 고려하면 방진 장치를 개발하거나 진동수준이 낮은 농작업기계를 개발하여 작업환경을 개선하는 조치가 필요하다고 생각한다. 그러므로 농작업기계에 대한 진동수준에 대한 종합적인 연구와 그에 대한 대책 마련이 지속적으로 수행되어야 할 것이다.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.3
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• pp.22-30
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• 2011

There is a many way of LPRE throttling methods, high-pressure-drop systems, dual-manifold injector, gas injection, multiple chambers, pulse modulation and movable injector components. Especially dual-manifold injector is essentially combines two fixed-area injectors into a common structure, with independent feed systems controlling flow to each injector manifold. In this paper, using indirect photography and liquid film thickness measurement with various injection pressure and tangential entry diameter to decide stability of spray over a wide thrust range in dual manifold injector.

• Journal of the Korea Institute of Information Security & Cryptology
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• v.7 no.2
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• pp.93-106
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• 1997

Summation generator is a real adder generator with maximum period, near maximum linear complexity and maximum order of correlation immunity. But this generator has been analyzed by a correlation attack(a kind of known-plaintext attack), which confers carry bits from output sequences of consecutive 0's or 1's. As methods of immunizing carry-output correlation, an immunized summation generator which exclusively-ORed summation generator output with output of a stage of LFSR was proposed. But the immunized generator reuses the output of LFSR by k-bit later and does not garantees maximum period in special case. In this paper we proposed an improved summation generator with 2-bit memory and analyzed it.

• Aerospace Engineering and Technology
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• v.4 no.2
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• pp.171-191
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• 2005

This Technical Memo(TM) was written for the purpose of determining the type of UHF-band power divider which is applicable to KSLV-1. For this, some different kinds of power divider are compared with there types and characteristics. And then, we select three types of power divider(which is Wilkinson power divider, Quadrature hybrid divider and Ring hybrid divider) and perform Schematic and Momentum simulation for finding the optimized characteristics. With this results, in order to demonstrate the selected power divider, we manufactured UHF-band power dividers using FR-4 epoxy plate. By the measured results, we obtain the similar results compare with simulation and fabrication. And Quadrature hybrid power divider is suitable to application to KSLV-1.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.13 no.9
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• pp.1837-1844
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• 2009

In this paper, the circuit of 2 variable ternary adder and multiplier circuit using current mode CMOS are implemented. The presented ternary adder circuit and multiplier circuit using current mode CMOS are driven the voltage levels. We show the characteristics of operation for these circuits simulated by HSpice. These circuits are simulated under $0.18{\mu}m$ CMOS standard technology, $5{\mu}A$ unit current in $0.54{\mu}m/0.18{\mu}m$ ratio of NMOS length and width, and $0.54{\mu}m/0.18{\mu}m$ ratio of PMOS length and width, and 2.5V VDD voltage, MOS model Level 47 using HSpice. The simulation results show the satisfying current characteristics. The simulation results of current mode ternary adder circuit and multiplier circuit show the propagation delay time $1.2{\mu}s$, operating speed 300KHz, and consumer power 1.08mW.

• Journal of the Korean Institute of Telematics and Electronics D
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• v.35D no.11
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• pp.31-37
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• 1998

Magnitude/phase controlling circuit which is composed of attenuator and phase shifter make phase/gain cross-coupling, so too much tuning time is needed to find optimum operation point. In this paper, vector attenuator which control magnitude and phase of input signals is proposed. Vector attenuator in past ignores phase variation characteristics of attenuator, but vector attenuator of this paper compensates phase variation characteristics of attenuator. This vector attenuator consists of 0$^{\circ}$/180$^{\circ}$ phase shifter and low phase shifting attenuator and so forth. A 0$^{\circ}$/180$^{\circ}$ phase shifter has 0$^{\circ}$/179.9$^{\circ}$ phase shifting characteristics at a center frequency 881 MHz and a low phase shifting attenuator has an attenuation of 25dB, within the limit of 3.6$^{\circ}$ phase shift and less than -20dB reflection characteristics at both input and output ports. The designed vector attenuator shows that cartesian coordinate plane of output signal space can be represented correctly.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.10
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• pp.102-111
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• 2004

The procedure of design and manufacture of sub-scale combustor using bipropellant swirl injector with external mixing for a liquid rocket engine are described. The results of cold flow test, ignition test and combustion test of the sub-scale combustor are also given in this paper. The sub-scale combustor uses liquid oxygen(LOx) and kerosene as propellants and has a injector head, an ablative material combustor wall and a water cooled nozzle. The injector head has LOx manifold, fuel manifold, fire face plate, one center swirl injector and 18 main swirl injectors. The cold flow, ignition and combustion tests were successfully performed without damage of combustor. Results of hot firing tests show that combustion efficiency meets the target of design and operations of start and stop cyclogram are stable and high frequency combustion instability does not occur.

• Resources Recycling
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• v.19 no.2
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• pp.3-9
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• 2010

In most coal fired power plants, fly ashes collected from each of hoppers in the electrostatic precipitator are transported and stored in a silo. However the properties of the fly ashes collected from each of hoppers in electrostatic precipitator varies with the distance of the collection field from the boiler. The more distance hopper gets fly ash with larger specific surface area. Therefore, in electrostatic precipitator the hopper itself is expected to have the effect of classifying fly ashes. This study examines the physical, chemical and mineralogical properties of fly ash, collected from each of hoppers attached to an electrostatic precipitator in the coal fired power plant and looks into the possibility of the electrostatic precipitator being used as a classifier. Also, the study reviewed the possibility of acquiring high quality fly ash.

• Journal of Satellite, Information and Communications
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• v.12 no.4
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• pp.67-71
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• 2017

A solar array is main electrical energy source for Low-Earth-Orbit(LEO) satellite. The solar array cannot generate electrical energy during eclipse period, a battery supply electrical energy to the satellite. The electrical power of the solar array is changed in accordance with operating voltage and the solar array has the maximum power point. The solar array regulator makes the solar array supply electrical energy to the satellite and charge the battery. The solar array is connected to the solar array regulator input and the battery is connected to the solar array regulator output. The solar array regulator consists 2 of 3 hot redundant. One solar array regulator contains 3 DC-DC converters, and the solar array regulator operates stably even if the failure occur in one DC-DC converter. In this paper, the solar array regulator, the battery and the solar array operation is analyzed when the failure occur in one DC-DC converter.