• 항공우주시스템공학회지
• /
• 제10권3호
• /
• pp.15-22
• /
• 2016

The on-board appendages of satellites with mechanical moving parts such as the fly-wheel, the control-moment gyro, the cryocooler, and the gimbal-type directional antenna can generate an undesirable micro-vibration disturbance, which is one of the main causes of the image-quality degradation that affects high-resolution observation satellites. Consequently, the isolation of the micro-vibration issue has always been considered as salient, and the micro-vibration is therefore the focus of this study wherein a complex system that can provide the dual functions of a guaranteed vibration-isolation performance and electrical energy harvesting is proposed. The vibration-isolation and energy-harvesting performances of the complex system are predicted through a numerical analysis based on the characteristics that are obtained from component-level tests. In addition, the effectiveness of the complex system that is proposed in this study is verified through an assembly-level functional-performance test.

• 전자공학회논문지
• /
• 제51권4호
• /
• pp.210-217
• /
• 2014

본 논문에서는 한 바퀴 구동 이동로봇, GYROBO,에 대한 제어를 실험적으로 수행하였다. 이전 자이로보는 제자리에서 밸런싱을 할 경우, 내부의 짐벌이 한 쪽으로 계속 회전하는 현상이 발생하여 결국 넘어지게 되는 결과를 초래하였다. 이 구조적 문제를 보완하여 균형 제어에 대한 실험적 연구를 수행하였다. 실험을 통해 구한 게인값을 사용하는 게인 스케줄링 방법을 통해 쏠리는 현상에 대한 해결방법을 찾았고, 자세제어를 더 안정화 시켰다. 또한 주행이 가능한지를 확인하기 위해 직선 경로 주행실험을 하였다.

• 한국기계가공학회지
• /
• 제19권4호
• /
• pp.85-92
• /
• 2020

Applications for the unmanned aerial vehicle (UAV) have expanded enormously in recent years. Of all its various technologies, the UAV's ability to take off and land in a moving environment is particularly required for military or oceanic usage. In this study, we develop a novel leveling platform that allows the UAV to stably take off and land even on uneven terrains or in moving environments. The leveling platform is composed of an upper pad and a lower mobile base. The upper pad, from which the UAV can take off or land, is designed in the form of a 2 degrees of freedom (DOF) gimbal mechanism that generates the leveling function. The lower mobile base has a four-wheel drive structure that can be operated remotely. We evaluate the developed leveling platform by performing extensive experiments on both the horizontal terrain and the 5-degree ramped terrain, and confirm that the leveling platform successfully maintains the horizontal pose on both terrains. This allows the UAV to stably take off and land in moving environments.

• 한국정보통신학회논문지
• /
• 제5권5호
• /
• pp.1025-1030
• /
• 2001

3D stabilizing system구현 전 단계로서, 본 논문에서는 vehicle의 운동 중에도 지정된 방향을 유지하는 2D stabilizing system을 제작하였다. 본 system을 controller로서 DSP TMS320F240을, rate gyroscope로서 vibratory rate gyro(Tokimec co. TFG -l60D), direct drive driver/motor로서 SD1015B52-1·SD1004C04-l/DM1015B·DM1004C, control algorithm로서 PI control을 이용 system을 구현하여 rate gyro를 이용, 발생 error를 보상하도록 하여 비교적 나은 안정화 결과를 얻었다.

• 한국항공우주학회지
• /
• 제34권6호
• /
• pp.75-82
• /
• 2006

틸트로터 항공기는 기존의 헬리콥터에 비해 두 배 정도 빠르고 비행 가능 영역은 수배에 이른다. 로터시스템을 틸팅(tilting)하여 전진비행하기 때문에 기존 헬기 블레이드에서 발생되는 전진면의 압축성 효과와 후퇴면의 실속을 방지하는 효과를 얻을 수 있다. 그러나 틸트로터 항공기에서는 훨플러터(whirl flutter)로 알려진 공탄성 불안정성으로 인해 최대 전진속도에 제한을 가지게 된다. 본 논문에서는 우선 로터시스템 자체의 공탄성 안정성에 대한 파라메트릭 연구를 수행하였고, 피치링크 강성, 짐발 스프링 상수, 원추각이 스마트무인기의 훨플러터 안정성에 미치는 영향을 CAMRAD II를 이용한 해석을 통해 고찰하였다.

• 한국소음진동공학회논문집
• /
• 제26권3호
• /
• pp.323-330
• /
• 2016

This paper describes real-time unbalance moment compensation method for line of sight(LOS) stabilization control systems. The factors of system inertia, frictions and unbalance moment affect the control accuracy of drive systems that are equipped to on the move(OTM) platforms requiring LOS stabilization function. In case of the unbalance moment among those factors is continuously changed as variation of relative angle between gravity vector and drive torque vector. Then, consideration of the effect in real-time is very complicate. Therefore, its effect should be designed to be minimized, however, designing it almost zero is impossible in real condition. In other words, it is hard to achieve target performance overcoming stability issue of highly unbalanced systems. To solve these problems, this paper proposes calculation method of unbalance moment by using measured sensor data for LOS stabilization control and its use for control compensation. Also, kinematical converting process and control structure for compensation are explained. The effectiveness of the proposed method as variation of unbalance moment is verified under simulation circumstance modeled by assuming LOS control system with 2-axis gimbal structure.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2014년도 추계학술대회 논문집
• /
• pp.893-899
• /
• 2014

X-band antenna has been widely used to effectively transmit the high resolution image data from the observation satellite to the ground station. To achieve above mission, X-band antenna is mainly composed of the 2-axis gimbal system using stepping motors and gears. However, the micro-vibration induced by the stepping motor actuation and the imperfect gear teeth alignment during this on-orbit operation is the main source of image quality degradation. In this paper, X-band antenna combined with a blade gear for micro-vibration isolation was suggested and investigated. The structural safety of the blade gear with low rotational stiffness was confirmed by structure analysis based on the derived torque budget. The isolation performance of the X-band antenna with the blade gear was verified through micro-vibration measurement test using the dedicated micro-vibration measurement device proposed in this study.

• Journal of Biosystems Engineering
• /
• 제36권3호
• /
• pp.171-179
• /
• 2011

Facing the current hikes of labor wage and high oil price, it is needed to have energy-saving machinery which also enables us precise farm operations. Thus, it was necessary to develop a safe machine which allows secure and pleasant works along orchard slopes. In this study, a lifting utility with balance-controlled platform was developed. The platform utility could maintain to level the workbench while driving along slopes. Even the machine body was driven at the tilt angle ranges of ${\pm}20^{\circ}$, the platform bench could be maintained within ${\pm}0.5^{\circ}$ of a gimbal angle. In addition, the machine lifted up to 2.0 m using an electric-hybrid driving mechanism with a low noise. A tandem hybrid power source was developed with a DC 72 V, 100 AH for the Deep-Cycle batteries, charged with 3.5 kW gasoline generator as an auxiliary power source. HST, which is one of the CVT's, was adopted as a transmission device, and a crawer track was used for the safety of the vehicle against tip-over. The maximum lifting height of platform was is 2,500 mm, and the maximum extendable width was 2,900 mm.

• International Journal of Aeronautical and Space Sciences
• /
• 제14권4호
• /
• pp.369-378
• /
• 2013

This paper presents a vision/LiDAR integrated navigation system that provides accurate relative navigation performance on a general ground surface, in GNSS-denied environments. The considered ground surface during flight is approximated as a piecewise continuous model, with flat and slope surface profiles. In its implementation, the presented system consists of a strapdown IMU, and an aided sensor block, consisting of a vision sensor and a LiDAR on a stabilized gimbal platform. Thus, two-dimensional optical flow vectors from the vision sensor, and range information from LiDAR to ground are used to overcome the performance limit of the tactical grade inertial navigation solution without GNSS signal. In filter realization, the INS error model is employed, with measurement vectors containing two-dimensional velocity errors, and one differenced altitude in the navigation frame. In computing the altitude difference, the ground slope angle is estimated in a novel way, through two bisectional LiDAR signals, with a practical assumption representing a general ground profile. Finally, the overall integrated system is implemented, based on the extended Kalman filter framework, and the performance is demonstrated through a simulation study, with an aircraft flight trajectory scenario.

• 정보저장시스템학회:학술대회논문집
• /
• 정보저장시스템학회 2005년도 추계학술대회 논문집
• /
• pp.47-52
• /
• 2005

A lot of information storage devices have been introduced and developed for recently years. The trends of those devices are high capacity, compact size, low power consumption, reliability, and removability for data interchange with other device. As a satisfaction of these trends, near-field technique is in the spotlight as the next generation device. In order for a near-field recording to be successfully implemented in the storage device, a slider and suspension is introduced as actuating mechanism. The optical slider is designed considering near-filed optics. Suspension is not only supports slider performance, and tracking servo capacity but also meets the optical characteristics such as tilt aberration, and guarantee to satisfy shock performances for the mobility fir the actuator. In this study, the optical slider and the suspension for near-field probe array are designed and analyzed considering dynamic performance of head-gimbal assembly and shock simulation..