• International Journal of Aeronautical and Space Sciences
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• 제17권1호
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• pp.120-131
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• 2016

The full results of troubleshooting process related to the flight control system of a tilt-rotor type UAV in the flight tests are described. Flight tests were conducted in helicopter, conversion, and airplane modes. The vehicle was flown using automatic functions, which include speed-hold, altitude-hold, heading-hold, guidance modes, as well as automatic take-off and landing. Many unexpected problems occurred during the envelope expansion tests which were mostly under those automatic functions. The anomalies in helicopter mode include vortex ring state (VRS), long delay in the automatic take-off, and the initial overshoot in the automatic landing. In contrast, the anomalies in conversion mode are untrimmed AOS oscillation and the calibration errors of the air data sensors. The problems of low damping in rotor speed and roll rate responses are found in airplane mode. Once all of the known problems had been solved, the vehicle in airplane mode gradually reached the maximum design speed of 440km/h at the operation altitude of 3km. This paper also presents a comprehensive detailing of the control systems of the tilt-rotor unmanned air vehicle (UAV).

• 제어로봇시스템학회논문지
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• 제16권9호
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• pp.905-912
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• 2010

Modern version of advanced supersonic fighter have ATCS (Automatic Thrust Control System) to maximum flight safety, fuel efficiency and mission capability the integrated advanced autopilot system such as TFS (Terrain Following System), GCAS (Ground Collision Avoidance System) and AARS (Automatic Attitude Recovery System) and etc. This paper addresses the design and verification of ATCS based on advanced supersonic trainer in HILS (Hardware In the Loop Simulator) with minimum hardware modification to reduce of development cost and maintain of system reliability. The function of ATCS is consisted of target speed hold mode in UA (Up and Away) and angle of attack hold mode in PA (Power Approach). The real-time pilot evaluation reveals that pilot workload is minimized in cruise and approach flight stage by ATCS.

• 전기전자학회논문지
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• 제23권2호
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• pp.606-613
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• 2019

본 논문에서는 파장 스위핑 레이저의 평탄 스위핑을 자동 유지하기 위한 새로운 방식을 제안하였다. 이 방식이 적용된 레이저의 제작 및 실험을 통하여 5시간이 경과하여도 평탄 스위핑 특성이 잘 유지되고 있음을 관찰하였다. 그리고 56nm의 스위핑 범위, 1kHz의 스위핑 주파수, 그리고 8.8mW 의 광 출력 파워도 확인하였다. 제안된 방식은 기존에 스위핑 레이저를 장시간 구동시킬 때 불가피하던 수동 편광 조절의 번거로움을 해소시키고 이 과정에서 요구되던 고가 광 스펙트럼 분석기의 사용을 배제시킨다.

• 제어로봇시스템학회논문지
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• 제20권11호
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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.

• Journal of Magnetics
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• 제8권4호
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• pp.160-163
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• 2003

In magnetic flux measurement, output voltage drift of electronic integrator is an essential problem. In this work, we have developed a new kind of Miller type integrator using a sample and hold amplifier. Input bias current was measured and this value was hold in the sample and hold amplifier, after that input bias current of Miller integrator was compensated automatically using the value which holds in the sample and hold amplifier. Developed flux-meter shows the drift of flux-meter are smaller than 10$^{-5}$ Wb/min in full scale of 10$^{-2}$, and we could also measure multi-channel magnetic flux simultaneously.

• 전자공학회논문지
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• 제51권4호
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• pp.193-200
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• 2014

본 논문에서는 방사성 의약품의 자동합성장치에 사용되는 단채널 감마선 분광기를 보드 형태로 설계, 제작하고 그 특성을 측정 분석하였다. 감마선 검출을 위해 CZT (CdZnTe) spear 검출기를 이용하였고 아날로그 방식을 적용한 신호처리 보드의 형태로 감마선 분광기를 제작하였다. 측정을 위하여 방사성 물질인 Co-60을 시료로 사용하였으며, 최대 1173keV까지의 감마선 에너지 스펙트럼을 얻을 수 있었다. 아날로그 보드는 CZT spear 검출기에서 감마선을 검출하여 출력하는 신호를 적절히 변화시켜주기 위한 SF (shaping filter) 및 PHA (peak and hold amplifier)와 수치화된 감마선 신호 데이터를 계산하기 위한 ADC(analog to digital converter)와 FPGA (field programmable gate array)로 구성되었다.

• 대한조선학회논문집
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• 제31권4호
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• pp.99-108
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• 1994

본 연구는 "유조선 구조해석을 위한 유한요소 입력자동화 프로그램의 개발"[1]의 연속된 연구결과로서, 유조선, 살물화물선, 콘테이너선등의 일반 상용 선박을 대상으로 유한요소법을 이용하여 선체중앙부(3-D cargo hold)구조해석을 수행할 때, 구조모델링과 해석을 위한 입력자료처리를 효율적으로 자동화하는 과정을 연구하였다. 본 논문에서는 전년도에 발표된 기본 알고리즘을 바탕으로 다양한 형태의 선종별 적용성, MSC/NASTRAN 인터페이스와 관련한 평면 유한요소 자동분할 기법, 파랑하중 직접계산 인터페이스 개발 및 입력자료 처리과정에 도입된 Graphic User Interface기법 등 새로이 개발된 내용에 대하여 자세히 기술하고, 다양한 실적선에 적용함으로써 프로그램의 유용성을 확인하였다.

• 대한조선학회논문집
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• 제58권5호
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• pp.303-313
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• 2021

Recently, quality control of the Liquefied Natural Gas Carrier (LNGC) cargo hold and block-erection interference areas using 3D scanners have been performed, focusing on large shipyards and the international association of classification societies. In this study, as a part of the research on LNGC cargo hold quality management advancement, a study on deep-learning-based scaffolding system 3D point cloud object detection and post-processing were conducted using a LNGC cargo hold 3D point cloud. The scaffolding system point cloud object detection is based on the PointNet deep learning architecture that detects objects using point clouds, achieving 70% prediction accuracy. In addition, the possibility of improving the accuracy of object detection through parameter adjustment is confirmed, and the standard of Intersection over Union (IoU), an index for determining whether the object is the same, is achieved. To avoid the manual post-processing work, the object detection architecture allows automatic task performance and can achieve stable prediction accuracy through supplementation and improvement of learning data. In the future, an improved study will be conducted on not only the flat surface of the LNGC cargo hold but also complex systems such as curved surfaces, and the results are expected to be applicable in process progress automation rate monitoring and ship quality control.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1999년도 하계학술대회 논문집 C
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• pp.1070-1072
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• 1999

Automatic Generation Control(AGC) is a control system whose objectives are to hold system frequency close to a specified nominal value and to maintain each unit's generation at the most economic value. It has been used to control the output of a generator by the control signal of the generator, but it is not appropriate to apply to generators which adopt the distributed control system. In this paper a method for improving the AGC operation is proposed, and the different response of each generator and various types of control systems of generators are considered. The interface among Remote Terminal Detector(RTU) and control systems and the direct delivery of the data between EMS and DCS also are proposed in the paper.

• 조명전기설비학회논문지
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• 제28권1호
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• pp.57-68
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• 2014

This paper propose a development of squirrel-cage induction motor(IM) for 5-phase 1.5kW, 220V, 60Hz in order to study a polyphase ac machinery that keep hold of advantages more than traditional three-phase a IM, such as reducing a amplitude of torque pulsation, decreasing electric noises, and increasing the reliability. Designed methods of the motor use a development tools with Maxwell 2D and Simplorer program. There are designed drawing of manufactured frames of the IM. amplitude and waveform of the generated electromotive force, FFT analysis of harmonics within output voltages and current, and reviewing a experiment results are shown by variable output. We are presenting a design and manufacture methods for the 5-phase squirrel-cage IM.