• International Journal of Aeronautical and Space Sciences
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• 제8권1호
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• pp.10-20
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• 2007

For spacecraft attitude control, reaction wheel (RW) steering laws with more than three wheels for three-axis attitude control can be derived by using a control allocation (CA) approach.1-2 The CA technique deals with a problem of distributing a given control demand to available sets of actuators.3-4 There are many references for CA with applications to aerospace systems. For spacecraft, the control torque command for three body-fixed reference frames can be constructed by a combination of multiple wheels, usually four-wheel pyramid sets. Multi-wheel configurations can be exploited to satisfy a body-axis control torque requirement while satisfying objectives such as minimum control energy.1-2 In general, the reaction wheel steering laws determine required torque command for each wheel in the form of matrix pseudo-inverse. In general, the attitude control command is generated in the form of a feedback control. The spacecraft body angular rate measured by gyros is used to estimate angular displacement also.⁵ Combination of the body angular rate and attitude parameters such as quaternion and MRPs(Modified Rodrigues Parameters) is typically used in synthesizing the control command which should be produced by RWs.¹ The attitude sensor signals are usually corrupted by noise; gyros tend to contain errors such as drift and random noise. The attitude determination system can estimate such errors, and provide best true signals for feedback control.⁶ Even if the attitude determination system, for instance, sophisticated algorithm such as the EKF(Extended Kalman Filter) algorithm⁶, can eliminate the errors efficiently, it is quite probable that the control command still contains noise sources. The noise and/or other high frequency components in the control command would cause the wheel speed to change in an undesirable manner. The closed-loop system, governed by the feedback control law, is also directly affected by the noise due to imperfect sensor characteristics. The noise components in the sensor signal should be mitigated so that the control command is isolated from the noise effect. This can be done by adding a filter to the sensor output or preventing rapid change in the control command. Dynamic control allocation(DCA), recently studied by Härkegård, is to distribute the control command in the sense of dynamics⁴: the allocation is made over a certain time interval, not a fixed time instant. The dynamic behavior of the control command is taken into account in the course of distributing the control command. Not only the control command requirement, but also variation of the control command over a sampling interval is included in the performance criterion to be optimized. The result is a control command in the form of a finite difference equation over the given time interval.⁴ It results in a filter dynamics by taking the previous control command into account for the synthesis of current control command. Stability of the proposed dynamic control allocation (CA) approach was proved to ensure the control command is bounded at the steady-state. In this study, we extended the results presented in Ref. 4 by adding a two-step dynamic CA term in deriving the control allocation law. Also, the strict equality constraint, between the virtual and actual control inputs, is relaxed in order to construct control command with a smooth profile. The proposed DCA technique is applied to a spacecraft attitude control problem. The sensor noise and/or irregular signals, which are existent in most of spacecraft attitude sensors, can be handled effectively by the proposed approach.

• 항공우주기술
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• 제13권1호
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• pp.55-62
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• 2014

비행종단수신기는 발사체 비행 중 발생할 수 있는 비정상 상태에 대비하여 비행을 중단시키는 지상 명령을 수신하는 장치이다. Secure 톤은 IRIG에서 규정한 7개의 음성 주파수 대역 톤 신호 중 2개의 톤을 조합하여 11개의 연속적인 부호로 명령 포맷을 구성한다. 한국형발사체 탑재를 고려해 개발 중인 비행종단수신기는 Secure 톤에 암호화 기능을 추가한 MHA 명령 방식을 적용하였다. 제작된 비행종단수신기의 성능 및 기능을 점검하기 위해선 동일한 규격의 RF 신호를 발생함과 동시에 수신기의 외부 출력 포트를 모니터링하고 RS-422 통신을 제어하며 시험 데이터 저장 기능을 제공하는 점검장비가 필요하다. 본 논문에서는 비행종단수신기 인터페이스 및 적용된 명령 방식에 대한 간략한 설명과 함께 LabVIEW 기반으로 제작된 점검장비의 하드웨어 구성, 소프트웨어 구현 및 기능 점검 결과에 대해 기술한다.

• 전자공학회논문지T
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• 제36T권1호
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• pp.41-50
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• 1999

브러시리스 직류전동기는 보수 유지의 용이성과 가제어성의 특성으로 인하여 자동화 공장에서 많이 활용되고 있다. 본 논문에서는 산업현장에서 고성능과 유용성을 가지는 정현파형 브러시리스 직류전동기의 속도제어 서보시스템을 설계하였다. 이 서보시스템은 전동기의 구동에 필요한 제어장치와 새로운 자동동조 PI제어 알고리즘에 의해서 구현되어진다. 주 제어기와 센서 신호처리부는 고속연산의 필요성과 설계의 적절성 때문에 DSP를 사용하였고, DSP에서 출력되는 속도지령을 정확히 추종하기 위해 하드웨어 PWM 전류제어기를 구현하였다. 실험 결과 지령치에 대한 빠른 응답과 지령치 변화에 따른 정상상태 응답이 오버슈트 없이 잘 수렴함을 확인 할 수 있었다.

• 한국통신학회논문지
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• 제29권7A호
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• pp.807-813
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• 2004

본 논문은 21세기 지식기반경제의 국제사회에서 경쟁할 수 있는 우리만의 강점기술을 전략적 선택으로 집중개발 필요성 증대에 따라 추진하게 된 ‘21세기 뉴-프론티어 연구개발사업’ 의 일환인 ‘스마트 무인기(Smart Unmanned Aerial Vehicle) 기술개발’ 에 해당되며, 이 중 스마트 무인기의 운용에 필요한 원격명령(Tele-Command)신호의 수신기능과 동시에 영상(Video)신호 및 원격측정(Tele-Metry)신호를 송신하는 기능 등을 수행하는 Ku-대역 탑재영상 송수신시스템을 설계하였다. 또한, 설계된 전체 통신시스템의 체계요구에 만족하기 위하여 이를 해석하였으며, 전체 시스템의 모듈별 시뮬레이션 및 제작을 통해 본 논문의 타당성을 보였다.

• 한국군사과학기술학회지
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• 제18권1호
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• pp.37-45
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• 2015

These days many systems use the gps signal to get their own position. Because it's cheap and accurate and convenient. But, the strength of gps signal is very weak and can be easily interrupted by GPS jamming and GPS spoofing. Normally, fighter can use DME, TACAN, etc to correct their position error when GPS is not working. But, many aircraft which does not have those kinds of hardware need to pay additional cost to get it. In this paper, we propose how to overcome GPS jamming and GPS spoofing by only using data link system. The main purpose of this paper is to make the data link protocol to get an exact position information of own unit at gps error environment.

• 전기의세계
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• 제18권6호
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• pp.33-45
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• 1969

The purpose of this paper is design the most important part of sequential control systems, that is, command-treatment part, from the signal-transformation point of view. An orderly procedure is developed by which for sequential control systems the experimental design method can be reduced to the rational design method. Important in this procedure are: 1. To make total block diagram of sequential control systems by determining input and output signals of command-treatment part. 2. To partition over-all block diagram by observing each output signal. 3. To design concretely minimum block diagram by using the operational block diagram. By applying the method for partitioning the circuit to the design, the design method for sequential control systems is organized and done rationally without the aid of experiece.

• 전력전자학회논문지
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• 제17권3호
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• pp.259-265
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• 2012

This paper introduces a method for design and implementation of a current controller for boost converter operating in continuous conduction mode (CCM) using a digital signal processor (DSP). A Proportional-Integral (PI) type current controller outputs an average voltage command for inductor, used in the input side of the boost converter, and the duty-ratio of PWM (pulse width modulation) signal for switching device is directly calculated from the average voltage command. The gains of the PI current controller are selected such that the current response characteristics are the same as those of a first-order low-pass filter. The proposed current control scheme is implemented using a DSP based on fixed-point math operations and an experimental study has been performed to validate the proposed method.

• 한국정밀공학회지
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• 제23권4호
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• pp.83-90
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• 2006

A robot manipulator is usually operated in two modes: free and constrained motion modes, depending on whether the robot is in contact with an environment or not. At the moment of contact, an impact occurs and can exert harmful effects to the robot or the object. In case of teleoperation, since a user may give an inadequately excessive velocity command to the slave due to insufficient visual information, the robot nay collide the object with an excessive speed and it possibly deteriorates the robot's performance causing vibrations and at worst, shortens its lifetime by its fracture. In this article, a new algorithm is proposed by introducing a command signal modification method on the basis of impedance control and validity of the proposed algorithm is demonstrated by performing simulations and experiments.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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• pp.274-274
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• 2000

In the future, the convenient speech command system will become an widely-using interface in automation systems. But the previous research in speech recognition didn't give satisfactory recognition results for the practical realization in the noise environment. The purpose of this research is the development of a practical system, which reliably recognizes the speech command of the registered users, by complementing an existing research which used the image information with the speech signal. For the lip-reading feature extraction from a image, we used the DWT(Discrete Wavelet Transform), which reduces the size and gives useful characteristics of the original image. And to enhance the robustness to the environmental changes of speakers, we acquired the speech signal by stereo method. We designed an economic stand-alone system, which adopted a Bt829 and an AD1819B with a TMS320C31 DSP based add-on board.

• 센서학회지
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• 제9권6호
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• pp.448-454
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• 2000

This paper describes the implementation of a multi-subject, multi-channel optical telemetry system for the short range measurement of electrocardiograms (EKGs) a system which receives command signals and transmits physiological signals to the external system using LED (Light Emitting Diode) and PD (Photodiode). This system decreases the dependency of power supply voltage to the CMOS IC chips and a new enforced synchronization technique using infrared bi-directional communication has also been proposed. The telemetry IC with the size of $5.1{\times}5.1mm^2$ has the following functions: receiving of command signal, initialization of internal state of all functional blocks, decoding of subject selection signal, time division multiplexing of 4-channel modulated physiological signals, transmission of modulated signals to external system, and auto power down control.