• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2014.10a
• /
• pp.245-246
• /
• 2014

에어컨의 실내기에서 발생하는 소음은 주로 회전하는 팬의 진동에 의하여 발생하게 된다. 이는 구조기인 소음으로 낮은 주파수특성을 갖고, 흡음이나 차음의 소음저감방법으로는 해결하기 어려운 특성을 가지고 있다. 본 연구에서는 벽걸이형 에어컨 원심팬에 발생하는 진동(sway motion)의 원인을 진동실험과 동역학 시뮬레이션을 통하여 규명하였다. 실험적인 측면으로는 시스템분석과 시그널분석을 통하여 원심팬 구성품의 물성치 및 동특성을 확보하였고, 해석적인측면으로는 실험으로 확보된 원심팬의 동특성을 바탕으로 동역학 시뮬레이션 모델을 수립하였다. 실험 및 동역학 시뮬레이션을 바탕으로 원심팬 진동의 원인을 규명하였고, 원심팬 진동의 원인은 원심팬과 모터축사이의 축정렬 불량임을 확인하였다. 이를 해결하고 진동을 저감하기위한 장치를 고안하고 실험을 통하여 진동저감효과를 확인하였다.

• The Bulletin of The Korean Astronomical Society
• /
• v.37 no.2
• /
• pp.186.1-186.1
• /
• 2012

저궤도관측위성에 사용되는 광학 카메라는 대기 상태에서는 물론이고 우주 환경을 모사하는 열진공챔버 내에서도 광학 시험을 수행한다. 광학시험 수행 시, 광학카메라의 변위 및 각도를 조정하기 위하여 짐발을 사용한다. 짐발에 기능을 수행하기 위하여 적용된 기어 및 모터 등의 구조로 인하여 외부 진동에 취약할 수 있으며, 이러한 경우에는 광학시험 수행에 많은 제약을 줄 수 있다. 따라서 광학챔버 짐발의 변위 및 각도 변경 뿐만 아니라 안정적인 자세를 유지하기 위하여 기준 이상의 고유진동수 등의 동특성을 가져야 한다. 본 논문에서는 짐발 및 대상 광학 카메라의 질량특성을 모사한 대상물을 설치한 상태에서 수행한 동특성 시험 결과 및 수행한 분석 결과를 정리하였다.

• Journal of the Korea Institute of Information and Communication Engineering
• /
• v.10 no.7
• /
• pp.1332-1337
• /
• 2006

In this paper, a noble second stage hetero-estimator is used for positioning error detection in mobile robot. Previous methods are either expensive in the case of positioning error correction or not able to detect positioning error. To overcome the latter shortage, the positioning error detection is performed using second stage hetero-estimator in motor model of mobile robot without any additional costs. A Kalman filter in the estimator gets the residual of motor current and an adaptive self-tunning filter checks the whiteness of the residual. Some simulation results show the possibility of the proposed method.

• Journal of the Korean Institute of Intelligent Systems
• /
• v.25 no.4
• /
• pp.405-411
• /
• 2015

This paper sugg ests speed measurement and control system desig n methods to drive the Wheel-in Motor that is transfer rotational force to the hub of the wheel and drives it directly. The dsPIC30F2010 16 bit microprocessor specified to motion controller is used as a intelligent controller. The minimum functions of dsPIC30F2010, system clock, PWM output, I/O, timer, communication, applicable to motor control are used and operating characteristics of hall signal measurement and control software functions are tested. Also the algorithm including PDFF speed control program was implemented using this software functions and show the experimental results..

• Aerospace Engineering and Technology
• /
• v.6 no.1
• /
• pp.114-119
• /
• 2007

This paper introduces modal test of the 2nd stage structure of KSLV-I which is composed to satellite, PLA(Payload Adapter), EB(Equipment Bay), KMS(Kick Motor Support) and KM(Kick Motor) without PLF(Payload Fairing). In this test, to simulate free-free boundary condition, test object was hung by 4 bungee cords and excited by using impact hammer. From this test, dynamic properties of the 2nd stage structure of KSLV-I can be obtained. Modal test data are analyzed by using TDAS(Test Data Analysis Software). As the result, modal parameters and mode shapes below 100Hz of the 2nd stage of KSLV-I were identified.

• Journal of Power System Engineering
• /
• v.6 no.3
• /
• pp.36-41
• /
• 2002

A swashplate type piston motor with a tripod joints is introduced to improve compactness and starting torque in conventional types of motor. If the driving torque of motor shaft is transmitted by utilizing the mechanism, its friction torque loss would be drastically reduced and mechanical efficiency would be improved because the lateral force on the piston of the rod type motor with tripod joints mechanism is relatively smaller than that of the conventional plunger type motor. In particular, kinematics analysis for the mechanism are done as a preliminary study to investigate the feasibility of the mechanism in the axial piston motor. General formulas are derived from the displacement and velocity analysis of the mechanism, showing relationships between output shaft and shoe holder motion. A series of numerical calculations are carried out for a medium size motor with 160cc/rev using the formulas and their graphical plots are shown as well.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.25 no.9
• /
• pp.1334-1340
• /
• 2001

In this paper, the experimental modeling of the force between permanent magnet and iron-core solenoid is suggested for more accurate control of 3 D.O.F. motor using the electromagnetic force. In the case of iron-core solenoid, the general equation of solenoid cant be used simply because of its nonlinearity. Therefore, the magnetic flux density is estimated through the concept of equivalent permanent magnet. The force distribution between permanent magnet and iron-core solenoid is more dependent on the magnetization of iron core caused by the permanent magnet than any other parameters. Therefore, the equation of the force estimation between these magnetic systems can be modeled by the experimental function of the magnetization of iron core. Especially, if the distance between iron-core solenoid and permanent magnet is far enough, the force equation through experiment can be expressed from only the current of coil and the distance between iron-core solenoid and permanent magnet. It means that Coulombs law can be used for magnetic systems and it is validated through the experiment. Therefore, force calibration is performed by the concept of Coulombs law.

• The Journal of Korea Institute of Information, Electronics, and Communication Technology
• /
• v.11 no.3
• /
• pp.295-300
• /
• 2018

Conventionally, a PI control algorithm has been widely used as a speed control algorithm for BLDC motor. The PI control algorithm has a disadvantage in that is slow to reach the steady state due to the slow speed and torque response with various speed changes. Therefore, in this paper, PWM fuzzy logic control algorithm which can reach the steady state quickly by improving the response speed although there is a little overshoot is proposed. PWM reduces response speed and fuzzy logic control algorithm minimizes overshoot. The proposed PWM fuzzy logic control algorithm consists of DC chopper, PWM duty cycle regulator, and fuzzy logic controller. The performance and validity of the proposed algorithm is verified by simulation with Simulink of Matlab 2018a.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2006.05a
• /
• pp.41-44
• /
• 2006

The propulsion system of VIA-50A airship consists of engine, generator, inverter, motor and propeller. The motor and propeller was designed that can be tilted to $120^{\circ}$ for thrust vector control. When the flight test was performed, various condition data of the airship were obtained by wireless telecommunication and analyzed in real-time. In this paper, we presented flight test results of propulsion system. Considering the designed requirement and normal range, we verified that all constituent part was operated in normal condition during the high altitude flight test.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2009.11a
• /
• pp.526-529
• /
• 2009

In this study, we analyze the characteristic of burning classified by a propellant according to a flux of an oxidizer to analyze propellant regression distance in accordance with a thrust control and burning time of hybrid rocket using hybrid combustor of Lab-Scale. To control a flux of an oxidizer, we design flow control system to regulate the mount of opening and shutting of a needle valve by a driving of stepping motor by a combination the needle valve with stepping motor. We derive the relationships between mass flow rate and regression rate according to a propellant through the oxidizer flux change. While doing the thrust control, we estimate regression distance through the oxidizer flux in accordance with thrust and confirm the creditability through the actual thrust control burning experimentation.