• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.7
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• pp.673-683
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• 2010

This study investigates Terrain Aided Inertial Navigation(TAIN) which consists of Inertial Navigation System (INS) with the optical sensor for precise planetary landing. Image processing is conducted to extract the feature points between measured terrain data and on-board implemented terrain information. The navigation algorithm with Iterated Extended Kalman Filter(IEKF) can compensate for the navigation error, and provide precise navigation information compared to single INS. Simulation results are used to demonstrate the feasibility of integration to accomplish precise planetary landing. The proposed navigation approach can be implemented to the whole system coupled with guidance and control laws.

• Journal of the Korean Institute of Telematics and Electronics S
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• v.35S no.10
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• pp.64-76
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• 1998

In this paper, we propose the dynamic modeling, path planning and tracking algorithms of 4-wheeled 2-d.o.f.(degree of freedom) mobile robot(WMR). The gaussian functions are applied to design the smooth path of WMR. To calculate the WMR position in real time, we use three components of inertial measurement units(IMU). These units have initial error because of the rotation rate of earth, gravity acceleration and so on. Therefore we derive the initial error model of IMU, and compare the fitness diagnosis about probability characteristics of real data adn estimated data. The performance of IMU with error model and Kalman filter is compared to that without filter and error model. The simulation results show that the proposed dynamic model, path planning and tracking algorithms are more useful than the conventional control algorithm.

• Journal of Advanced Marine Engineering and Technology
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• v.40 no.9
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• pp.743-748
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• 2016

Ship's diesel engines have intrinsic problem to make vibrations caused by cylinder explosion and unbalanced rotating mass. These vibrations might induce noises, are transferred to hull and neighboring structures and cause secondary vibrations. This paper suggests the use of an additional dynamic absorber with a sub-vibration system to reduce the aforementioned vibrations. This dynamic absorber is designed based on an analysis of the free vibration of the engine shafting system and the forced vibrations.

• Proceedings of KOSOMES biannual meeting
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• 2018.06a
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• pp.82-82
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• 2018

• Proceedings of the Korea Air Pollution Research Association Conference
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• 2001.11a
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• pp.431-432
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• 2001

원심력을 이용한 대표적인 대기오염 방지 장치인 싸이클론은 1800년대 후반이래 공기나 배출가스로부터의 분진제거 및 입자분리에 폭 넓게 사용되어 왔다. 일반적으로 싸이클론은 간단한 구조로 되어 있으며, 조작이 용이하고 운전비용이 저렴할 뿐만 아니라 가혹조건에서의 사용이 가능하다는 장점이 있다 (Shepherd and Lapple, 1939). 입자의 관성력에 의해 분진을 분리하는 싸이클론으로서는 상대적으로 낮은 관성효과를 지니는 미세입자(주로 10$\mu\textrm{m}$ 이하)들에 대한 제어효율이 낮을 수 밖에 없다(Dirge and Leith, 1985). (중략)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.6
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• pp.438-445
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• 2019

In this paper, we present a new approach to extract the g-sensitivity scale-factor error for a MEMS gyroscope. MEMS gyroscopes, based on the use of both angular momentum and the Coriolis effect, have a g-sensitivity error due to mass unbalance. Generally, the g-sensitivity error is not considered in general use of gyroscopes, but it deserves our attention if we are to develop for tactical class performance and reliability. The g-sensitivity error during vehicle flight increases navigation error; so it must be analyzed and compensated for the use of MEMS IMU for high dynamics vehicle systems. Therefore, we analyzed how to extract the g-sensitivity scale-factor error from the inertial sensor error model. Furthermore we propose a new method to extract the g-sensitivity error using flight motion simulator. We verified our proposed method with experimental results.

• Transactions of the Korean Society of Automotive Engineers
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• v.15 no.6
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• pp.114-119
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• 2007

Because the small trailers do not have the main brake system, it is difficult to gain the effective braking performance of the trailers while driving them. Especially it is very hard to brake them on the slope road condition. So we have technically developed Inertia Braking System for the military trailers which have not main braking system. Inertia Braking System is designed to be activated by the inertia force of trailer. It consists of the brake rod, damping cylinder, hand brake lever and brake cables. We have tested the trailer's braking performance. As a result, we have showed that the trailer's braking performance of the trailer equipped with Inertia Braking System, the road driving performance and the braking safety capability are improved dramatically. And we hope that it is rare to happen the accident while driving.

• Proceedings of the Korean Institute of Intelligent Systems Conference
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• 2006.05a
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• pp.343-346
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• 2006

스마트 홈서비스가 이루어질 앞으로의 가정에서는 거주자의 편리를 추구하는 다수의 가전기기와 다양한 장치를 통해 여러 형태의 서비스가 제공된다. 그 환경의 중심에서 사용자는 무엇보다 손쉽고 편리하게 이들을 시용할 수 있어야 한다. 기존에는 사용자가 쉽게 휴대할 수 있는 소형 컴퓨터, PDA, 휴대폰을 이용해 스마트 홈서비스를 제어하는 연구가 이루어지고 있다. 하지만 이들을 사용하는 것은 복잡하면서 전문적인 지식이 필요할 수 있으며 항상 결에 두어야 한다는 불편함이 있을 수 있다. 이에 본 논문에서는 관성센서를 이용한 동작인식 시스템을 개발하였다. 이 시스템은 자이로 센서와 가속도 센서를 사용하며 3축의 자이로(각속도) 및 가속도를 측정할 수 있는 센서 모듈과 측정된 데이터를 이용해서 동작 패턴을 분류해 주는 알고리즘으로 구성된다. 차후에 홈 네트워크 시스템과의 결합을 통해 미리 지정된 간단한 손동작만으로 여러 가전기기를 제어할 수 있을 것이며 특히 노약자나 장애인들이 기존의 리모트 컨트롤 등의 복잡한 제어 장치를 대신해서 간편하고 손쉽게 사용할 수 있을 것이다.

• Journal of the Korea Institute of Military Science and Technology
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• v.12 no.3
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• pp.368-377
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• 2009

In this paper we study the gyro bias calibration method of SDINS(Strap-Down Inertial Navigation System). Generally, SDINS's calibration is performed in 2-axis(or 3-axis) rate table with chamber for varying ambient temperature. We assumed that the majority of calibration-parameter except for gyro bias is knowned. During gyrobias calibration procedure, it can be induced some disturbances(accelerometer's short-term error induced rate table rotation and anti-vibration mount's rotation). In these cases, old gyro-bias calibration methods(using velocity error or attitude error) have an error, because these disturbances are not detectable at the same time. So that, we propose a new gyro-bias calibration method(heading error minimizing using equivalent linear transformation) that can detect anti-vibration mount's rotation. And we confirm efficiency of the new gyro-bias calibration method by simulation.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2017.11a
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• pp.142-143
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• 2017

증강 현실에 대한 관심이 높아지면서, 물체를 자연스럽게 증강시키는 기술이 주목받고 있다. 그 방법 중 하나는 실제 물체처럼 수평면 위에 증강시키는 것이다. 본 논문에서는 카메라 영상과 관성 측정 장치(IMU: inertial measurement unit)를 사용해 물체를 증강시키기 위한 수평면을 찾는 방법을 제안한다. 우선, 수평면을 결정하는 데 기준이 될 3 차원 공간 좌표를 계산하기 위한 방법을 설명한다. 그리고 계산된 좌표들을 바탕으로 수평면을 찾는 방법을 제시한다. 제안한 방법을 사용하면 지면 방향을 이용하기 때문에 증강된 물체가 실제 물체처럼 서있게 할 수 있다.