• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.5
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• pp.437-444
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• 2010

This paper deals with the attitude control of an underactuated spacecraft that has one single-gimbal variable-speed CMG. An underactuated spacecraft may not converge to arbitrary attitudes if its total angular momentum is not zero. To stabilize a spacecraft, the CMG has to align with the angular momentum in the inertial frame. Four different install configurations for the CMG have been considered and controllable angular momentums have been analyzed. Also, based on the backstepping method, stabilizing control laws have been presented and their properties have been compared.

• Journal of the Korean Society of Manufacturing Technology Engineers
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• v.9 no.4
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• pp.147-153
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• 2000

This paper presents a design method using CAE(Computer Aided Engineering ) with the consideration of reliability for optimal gear driving system. This method considered a configuration of the intermediate shaft. There are four mounting types, such as double straddle, double overhung, output gear overhung, and input ger overhung in the intermediate shaft. The reliability and life analysis are based on the two-parameter Weigbull distribution lives of the gears and bearing . The validity and feasibility of the proposed method are verified by the application to transmission of a industry machine.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2010.05a
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• pp.563-564
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• 2010

• Journal of Power System Engineering
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• v.8 no.4
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• pp.24-30
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• 2004

In this study, a position synchronous control algorithm applied to two-axes pneumatic cylinder driving apparatus is proposed. The position synchronous control algorithm is composed of position controller and synchronous controller. The position controller is designed to minimize the effect of several nonlinear characteristics peculiar to the pneumatic cylinder driving apparatus on position control performance. The synchronous controller is designed to reduce the synchronous error. The effectiveness of the proposed controller is proved by simulation results.

• Journal of Advanced Marine Engineering and Technology
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• v.38 no.6
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• pp.648-657
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• 2014

This paper is about the study on a newly developed small waterproofed 4-axis robot arm and the analysis of its kinematics and dynamics. The structure of robot arm is designed to have Pitch-Pitch-Pitch-Yaw joint motion for inspection using a camera on itself and the joint actuator driving capacity are selected and the joint actuators are designed and test for 10m waterproofness. The closed-form solution for the robot arm is derived through the forward and inverse kinematics analysis. Also, the dynamics model equation including the damping force due to the mechanical seal for waterproofness is derived using Newton-Euler method. Using derived dynamics equation, a sliding mode controller is designed to track the desired path of the developed robot arm, and its performance is verified through a simulation.

• Proceedings of the Korea Information Processing Society Conference
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• 2023.11a
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• pp.1145-1146
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• 2023

모빌리티 기술이 발전함에 따라 기존 차량에서 선보이지 못했던 다양한 주행기술이 가능해졌고, 이에 따라 많은 장점을 지닌 모빌리티 기술들이 등장하고 있다. 4 륜 독립 구동, 제동, 조향 시스템은 바퀴 별 독립 제어가 가능하여 여러 주행 모드를 구현할 수 있다. 본 연구에서는 4 륜 독립 구동, 제동과 독립 조향이 가능한 모빌리티 플랫폼에 대해 평행 주행, 제자리 회전, 축 회전 주행 등을 구현하는 방안과, 더 나아가 각도 속도를 일정하게 유지함으로써 오차를 최소화하는 제어 방법에 대해 살펴보고자 한다.

• Proceedings of the KIPE Conference
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• 2011.07a
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• pp.561-562
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• 2011

인 휠 모터를 이용하여 구동되는 전기차량은 각 모터의 동기 제어가 요구된다. 기존의 마이크로컨트롤러는 구동시킬 수 있는 모터의 개수가 제한되어 인 휠 모터를 이용하여 구동되는 전기차량과 같은 다축 제어 시스템에 적용하기가 어렵다. 따라서 본 논문에서는 FPGA(Field Programmable Gate Array)를 이용하여 4축 동기 SVPWM 기법을 구현하였으며, 시뮬레이션을 통하여 성능을 확인하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.4
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• pp.30-35
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• 2009

Effective-pivot effects on the thrust vector control performance of the flexible seal nozzle to be used to control the flight direction of missile were investigated by computer simulation. $2^3$-Design of experiment technique was applied and ADMAS was used for the surrogate technique. As a result, radial pivot position had more influence upon the nozzle actuating performance than axial pivot position. Connecting method of actuator was also important factor in determining effective-pivot effects on the thrust vector control performance of the flexible seal nozzle.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.14 no.5
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• pp.466-471
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• 2003

In this paper, we introduce a new photodetector configuration that automatically aligns its receiving angle to the incident signal light. Around the central photodiode that receives the optical signal, 4 photodiodes on ${\Phi}$-axis and 2 photodiodes on $\theta$-axis are installed in order to drive 2 step motors in f and $\theta$ direction. The photodetector completes angle-alignment within Isec to the signal light from an arbitrary direction.

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.1
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• pp.68-75
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• 2015

In this paper, unsteady characteristics of pressure in solid rocket motor were analyzed by using response of pintle actuation, pressure and thrust data from ground test. Pressure and thrust in solid rocket motor can be controlled in real time by varying nozzle throat area with pintle, installed in the valve. Unsteady characteristics of pressure can be observed in this system occurred by various reasons. Two critical reasons, error of pintle actuation and ablation of center tube, are found and effects of each reason can be analyzed individually by re-prediction of pressure with response of pintle actuation and analyzing thrust to pressure ratio.