• Journal of Advanced Navigation Technology
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• v.27 no.6
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• pp.763-769
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• 2023

Flight control computers for unmanned aerial vehicles are avionics that require high reliability and are generally designed to be multiplexed for margins on failures. The multiplexed flight control computer should include an interface through discrete signals and CCDL for synchronization and fault separation between channels. With the development of unmanned aerial vehicle technology, various types of platforms such as AAM and LPI are being developed in the private and military, which require advanced control performance for high-performance flight control and SWaP optimization of onboard equipment. In this paper, we designed a optimized flight control computer architecture for unmanned aerial vehicles for multiplexing processing and performed a software design for input and output control. In addition, input/output processing performance was evaluated through the implemented flight control computer and input/output software.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.17 no.12
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• pp.1333-1342
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• 1992

This paper deals with a robot manipulator having actuator which is described by equation $D(q)\ddot{q}=u-P(q\;\dot{q},\;\ddot{q})$ where u(t) is a control input. We employ two steps of controller design procedures. First, a global linearization is performed to yield a decoupled controllable linear system. Then a controller is designed for this linear system. We provide a rigorous analysis of the effect of uncertainty of the dynamics, which we study using robustness results in time domain based on a Lyapunov equation and the total stability theorem. Using this approach we simulate the performance of controller of a robot manipulator.

• The Journal of the Acoustical Society of Korea
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• v.7 no.2
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• pp.5-19
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• 1988

The feedback controllers for the active vibration control of elastic systems are developed using optimal regulator, optimal tracking, time optimal and noise observer algorithms. Using the modal analysis of the elastic systems, the effects of the actuator positions, the input weighting factor and the magnitude of the constraint of the actuator force are investigated.

• Proceedings of the KIEE Conference
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• 2000.07d
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• pp.2892-2894
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• 2000

인터넷을 이용한 원격 제어에 있어서는 통신 프로토콜은 TCP/IP를 기반으로 이루어지고 있는데 대개의 경우는 소켓을 이용한 PC기반에서 해석되어 지고 처리되어 진다. 본 논문에서는 PC기반의 원격제어 시스템을 임베디드화함으로써 시스템의 안정성과 속도면에서 우수한 시스템을 구현하려고 한다. 이를 위하여 임베디드 시스템은 HD860-R3보드를 이용하였고 실시간 운영체제로 리눅스를 사용하였다 실질적인 제어물의 제어를 위해서 제어기를 설계 HD860-R3보드와 시리얼을 통하여 통신하였다. 나아가 이 시스템을 PC기반의 시스템에서 탈피한 시스템을 홈 오토메이션의 제어 시스템에 적용시켜 보려 한다.

• Proceedings of the KIPE Conference
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• 2014.07a
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• pp.357-358
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• 2014

본 논문에서는 태양광 모듈의 최대 전력점을 추종하기 위한 제어 기법으로 부스트 컨버터(boost converter)의 불연속 전류모드(Discontinuous Current Mode)에서 주파수를 제어하는 기법을 구현 하였다. 태양광 모듈에 연결된 부스트 컨버터는 전압루프를 통하여 Perturb and Observation(P&O)기법을 사용하여 최대 전력점을 추종하였다. 부스트 컨버터의 인덕터에 흐르는 전류는 불연속 전류모드로 제어 된다. 불연속 전류모드에서의 제어기 설계는 MATLAB과 PSIM의 전달함수특성을 수학적 모델링을 통하여 비교 검증 하였으며, 모든제어는 MCU(TEXAS INSTRUMENTS사의 DSPF28335)를 통해 디지털로 제어 하였다. 제안된 기법은 단일 PV모듈이 연결된 불연속전류모드 부스트 컨버터를 통해 동작특성을 분석하였다.

• Cement Symposium
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• no.29
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• pp.42-49
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• 2002

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.1
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• pp.76-81
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• 2009

A nonlinear pressure controller to actively regulate the thrust of a solid propulsion system is presented. To compensate for the parametric uncertainties with respect to the chamber pressure induced by changing nozzle throat area, Lyapunov-based parameter adaptation method has been applied. In order to verify the effectiveness of the proposed control method, the experiments were carried out using the cold gas test equipment that can simulate the operating environment of variable thrust solid propulsion system. The experiment results show that the nonlinear pressure controller has better performance than conventional P and PI controller.

• Proceedings of the Korean Powder Metallurgy Institute Conference
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• 1997.10a
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• pp.20-20
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• 1997

• Proceedings of the Korean Magnestics Society Conference
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• 1994.10a
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• pp.36-37
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• 1994

• Proceedings of the Korean Fiber Society Conference
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• 2001.04a
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• pp.333-337
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• 2001