• Journal of the Korean Institute of Intelligent Systems
• /
• v.25 no.4
• /
• pp.398-404
• /
• 2015

In this paper, we describe the design and performance of a prototype multi-rotor unmaned aerial vehicle( UAV) platform featuring an inertial measurement unit(IMU) based autonomous-flying for use in bluetooth communication environments. Although there has been a fair amount of study of free-flying UAV with multi-rotors, the more recent trend has been to outfit hexarotor helicopter with gimbal to support various services. This paper introduces the hardware and software systems toward very compact and autonomous hexarotors, where they can perform search, rescue, and surveillance missions without external assistance systems like ground station computers, high-performance remote control devices or vision system. The proposed system comprises the construction of the test hexarotor platform, the implementation of an IMU, mathematical modeling and simulation in the helicopter. Furthermore, the hexarotor helicopter with implemented IMU is connected with a micro controller unit(MCU)(ARM-cortex) board. The micro-controller is able to command the rotational speed of the rotors and to get the measurements of the IMU as input signals. The control simulation and experiment on the real system are implemented in the test platform, evaluated and compared against each other.

• Journal of the Korean Institute of Intelligent Systems
• /
• v.21 no.4
• /
• pp.518-524
• /
• 2011

This paper presents a study on the calibration of accelerometer data in the gyroscope free inertial navigation system(GFINS) using fuzzy inference system(FIS). The conventional INS(inertial navigation system) which can measure yaw rate and linear velocity using inertial sensors as the gyroscope and accelerometer. However, the INS is difficult to design as small size and low power because it uses the gyroscope. To solve the problem, the GFINS which does not have the gyroscope have been studied actively. However, the GFINS has cumulative error problem still. Hence, this paper proposes Fuzzy-GFINS which can calibrate the data of an accelerometer using FIS consists of two inputs that are ratio between linear velocity of the autonomous ground vehicle(AGV) and the accelerometer and ratio between linear velocity of the encoders and the accelerometer. To evaluate the proposed Fuzzy-GFINS, we made the AGV with Mecanum wheels and applied the proposed Fuzzy-GFINS. In experimental result, we verified that the proposed method can calibrate effectively data of the accelerometer in the GFINS.

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 1991.11a
• /
• pp.49-53
• /
• 1991

최근 단위 시간당 생산성 향상을 위한 기계적 시스템의 작업속도가 계속적으로 증가되고 있으며, 그에 따라 관성력과 모터의 회전 토오크를 줄이기 위하여 시스템을 구성하고 있는 요소들의 구조 경량화 작업이 필요하게 되었다. 따라서 종래의 해석이론을 벗어난 메카니즘의 동탄성해석에 대한 중요성이 대두되었고, 이는 특히 기계의 작동속도에 대한 공진현상 및 위치 정확도와 밀접한 관계가 있기 때문에 품질향상면에 있어서 매우 중요하게 인식되고 있다.(중략)

• Proceedings of the KIEE Conference
• /
• 2009.07a
• /
• pp.1648_1649
• /
• 2009

BLDC는 낮은관성, 빠른응답, 높은 전력밀도, 높은 신뢰성 및 유지보수를 요구하지 않기 때문에 산업용 어플리케이션에 널리 이용되고 있다. BLDC는 종래의 영구자석 DC모터의 운영 특성을 보이고 있지만 기계적인 정류자와 브러쉬를 제거 하였다. BLDC의 경우 자속이 일정하기 때문에 속도 제어가 중요하다. 회전자의 속도를 제어하기 위해 전류 지령치를 퍼지 뉴럴 네트워크를 이용하여 제어치를 추정한다.

• Bulletin of the Korean Space Science Society
• /
• 2004.04a
• /
• pp.61-61
• /
• 2004

과학기술위성 1호(STSAT-1)는 위성의 자세를 제어하기 위하여 Reaction Wheel Assembly(RWA)를 적용하였으며, 위성의 무게중심에 Wheel의 회전수에 비례하는 관성모멘트를 발생시켜 자세를 제어하였다. 과학기술위성 2호(STSAT-2)는 과학기술위성 1호에 적용하였던 반작용휠(RWA)과 펄스형태로 동작시켜 위성의 자세 및 궤도제어를 위하여 요구하는 추력을 얻을 수 있는 펄스형 전기 추진시스템(Pulsed Plasma Thruster: PPT)이 탑재된다. (중략)

• Proceedings of the Computational Structural Engineering Institute Conference
• /
• 2003.04a
• /
• pp.348-354
• /
• 2003

This study outlines the analysis of toggle system and the vibration control performance when the toggle-rotational inertia damper system was applied to a structure. Numerical analysis shows that the relative displacement of the structure can be amplified by amplification mechanism of the toggle system and the capacity of the damper can be reduced without the loss of vibration control performance. It is also observed that vibration control effects is caused by the increase of equivalent mass due to the rotational inertia of damper.

• Proceedings of the Computational Structural Engineering Institute Conference
• /
• 2006.04a
• /
• pp.675-680
• /
• 2006

This paper deals with the flexural free vibrations of strip foundations. Based on dynamic equilibrium equations of a beam element resting on Winkler foundation, differential equations governing free vibration of strip foundation are derived, in which effects of rotatory inertia and shear deformation are included. For obtaining the natural frequencies, differential equations are solved by numerical methods. As the numerical results, relationships between natural frequencies and various strip parameters are obtained and presented in Tables and Figures.

• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
• /
• 1998.10a
• /
• pp.203-211
• /
• 1998

ER clutch is a device using electro-rheological fluid which is one of so called intelligent materials. Power transmission behavior of an ER clutch can be controlled by electrical field applied tb the fluid. In this work, a new type of servomechanism is developed with two ER clutchs, driven by two electrical motors rotating in reverse directions. The concentric cylinder type ER clutch is operated by PID control. The system shows good angular position control characteristics with respect to sinusoidal and square inputs.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 1997.10a
• /
• pp.110-115
• /
• 1997

A modeling method for the bending vibration analysis of rotating Timoshenko beams with concentrated mass and mass moment of inertia is presented. The shear and rotary inertia effects become critical for the accurate estimation of the natural frequencies and modeshapes as the slenderness ratio decreases. The effect of the concentrated mass and mass moment of inertia on the natural frequencies are also investigated with the modeling method.

• The Proceedings of the Korean Institute of Illuminating and Electrical Installation Engineers
• /
• v.4 no.3
• /
• pp.59-65
• /
• 1990

전력 전자 공학의 발달에 의해 영구자석 동기전동기의 운전 분야가 대단히 진보되고 있음이 최근 논문을 통해서 보고 되고 있다. 영구자석 동기전송기는 크기와 중량의 감소, 저관성, 고효율 등의 장점이 있어 각종 분야의 응용에 유리하다. 본 연구는 마이크로프로세서와 전압원 인버터를 사용한 자기제어현 영구자석 동기전송기의 구동장치를 제안한다. 영구자석 동기전동기의 운전 회전자 위치를 정확히 검출하여 회전자 속도와 운전주파수를 동기화 시킴으로서 자기제어를 가능하게 한다. 고 분해능의 인크리멘탈 엔코더를 사용하여 영구자석 동기전동기에 적합한 자기제어형 PWM인버터 설계를 가능하게 하였다. 저속 영역에서 토오크 리플을 감소시키기 위해 펄스 수를 제어하였다.