• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 춘계학술대회 논문집
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• pp.593-598
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• 2009

In this study we present results for the design of ground test system for 4 degree of freedom(DOF) control test is one of the smart UAV ground test. This system is equipped with real smart UAV and Z direction DOF and 3 direction rotation DOF, Ensuring safe operation of the Smart UAV is a top priority. To this end, it is required to do structure analysis and test verification to confirm the design margin and safety. Based on the analysis, the ground test system has been redesigned to meet the structural conditions.

• Smart Structures and Systems
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• 제7권4호
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• pp.303-317
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• 2011

A specially designed tendon, which is proposed by embedding an FBG sensor into the center king cable of a 7-wire strand tendon, was applied to monitor the prestress force and load transfer of ground anchor. A series of tensile tests and a model pullout test were performed to verify the feasibility of the proposed smart tendon as a measuring sensor of tension force and load transfer along the tendon. The smart tendon has proven to be very effective for monitoring prestress force and load transfer by measuring the strain change of the tendon at the free part and the fixed part of ground anchor, respectively. Two 11.5 m long proto-type ground anchors were made simply by replacing a tendon with the proposed smart tendon and prestress forces of each anchor were monitored during the loading-unloading step using both FBG sensor embedded in the smart tendon and the conventional load cell. By comparing the prestress forces measured by the smart tendon and load cell, it was found that the prestress force monitored from the FBG sensor located at the free part is comparable to that measured from the conventional load cell. Furthermore, the load transfer of prestressing force at the tendon-grout interface was clearly measured from the FBGs distributed along the fixed part. From these pullout tests, the proposed smart tendon is not only expected to be an alternative monitoring tool for measuring prestress force from the introducing stage to the long-term period for health monitoring of the ground anchor but also can be used to improve design practice through determining the economic fixed length by practically measuring the load transfer depth.

• 항공우주기술
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• 제9권1호
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• pp.1-8
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• 2010

스마트무인기의 비행시험에 앞서 비행제어시스템을 포함한 전체 무인기 체계의 건전성을 검증하기위한 지상통합시험을 수행하였다. 지상통합시험은 비행체 인터페이스 시험, 비행체 HILS시험, 지상파워시험, 4자유도 치구시험, 안전줄 호버시험 순서로 진행되었으며, 각각의 시험을 통해 전체 무인기 시스템의 안전성을 입증하였다. 본 논문에서는 국내 최초로 개발된 틸트로터인 스마트무인기의 지상시험 절차와 각 시험에서 획득한 데이터 분석결과를 제시하였다. 지상시험 결과 비행제어시스템의 안전성이 충분히 입증되었으며, 비행시험이 수행가능하다고 판단되었다.

• 한국군사과학기술학회지
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• 제13권1호
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• pp.22-29
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• 2010

In this study, computational multi-body dynamics and structural vibration analyses including some impact condition have been conducted for the ground flight test system of the developed smart UAV model. Designed ground test system has four degree-of-freedom motions with limited motion control mechanism. Design safety margin designs for several structural components are tested and verified considering expected critical motions (pitching and rolling) of the test smart UAV model. Computational results for various analysis conditions are practically presented in detail. Futhermore, proper design modifications of the initially designed test equipment in order to guarantee or increase structural safety have been successfully conducted in the design stage.

• Smart Structures and Systems
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• 제13권2호
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• pp.319-341
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• 2014

A family of smart tuned mass dampers (STMDs) with variable frequency and damping properties is analyzed under harmonic excitations and ground motions. Two types of STMDs are studied: one is realized by a semi-active independently variable stiffness (SAIVS) device and the other is realized by a pendulum with an adjustable length. Based on the feedback signal, the angle of the SAIVS device or the length of the pendulum is adjusted by using a servomotor such that the frequency of the STMD matches the dominant excitation frequency in real-time. Closed-form solutions are derived for the two types of STMDs under harmonic excitations and ground motions. Results indicate that a small damping ratio (zero damping is the best theoretically) and an appropriate mass ratio can produce significant reduction when compared to the case with no tuned mass damper. Experiments are conducted to verify the theoretical result of the smart pendulum TMD (SPTMD). Frequency tuning of the SPTMD is implemented through tracking and analyzing the signal of the excitation using a short time Fourier transformation (STFT) based control algorithm. It is found that the theoretical model can predict the structural responses well. Both the SAIVS STMD and the SPTMD can significantly attenuate the structural responses and outperform the conventional passive TMDs.

• 한국군사과학기술학회지
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• 제15권3호
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• pp.257-265
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• 2012

This paper presents a study on characteristics of precession motion of a smart munition. It's a kind of the Sensor Fuzed Weapon. The particular thing for the smart munition is that it has precession motion in the air while the sensor is searching the ground to detect ground vehicles such as tanks. The smart munition has a cylindrical shape and has a sensor attached on its side. Due to its non-uniform mass distribution, its center of gravity(CG) is located away from the center of volume(CV). In order for the smart munition to detect the target effectively, the ground searching pattern of sensor should have an uniform circular form, and for this, the precession motion of smart munition should be in its steady-state. Finally, it is necessary to choose the right initial conditions at the moment of firing, for the steady-state precession motion during flight.

• 시스템엔지니어링워크숍
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• 통권4호
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• pp.17-22
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• 2004

This paper present the brief generation process of system requirements or mart UAV from a development obejective. The current Snart UAV requirements deal with the restricted life cycle from development to test and verification exclusive of full life cycle beacuse of the new technology demonstration research program funded by goverments. The Smart UAV system consists of flight vechicle, avionics, communication link, payload, ground control stationand ground supporting system. In thus paper, top-down flown requirememts are intoduced how to allocate to each sub-system.

• 한국인터넷방송통신학회논문지
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• 제19권6호
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• pp.65-71
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• 2019

기존의 대지저항률과 접지저항 현장 측정 방식은 일정한 간격의 측정전극을 설치하여 전류를 인가하여 대지의 저항값에 따른 전압강하를 측정하게 되는데 현장 대지의 층상 구조가 특이성을 갖게 되면 역산 시 경계 조건의 오차를 발생하게 되고 접지 설계 시 중요한 대지저항률 분석이 시뮬레이션 상과 많은 차이를 보이게 된다. 본 연구는 정보통신 융합환경에서 아두이노 모듈과 스마트 접지 측정 기술를 활용하여 대지의 층상이 특이성을 갖는 구조라도 신뢰할 수 있는 스마트 대지 저항 측정장치를 개발하여 대지저항을 분석하고 데이터를 축적하여 대지의 경년변화를 예측한다. 현장의 지형적인 특성을 고려하여 접지저항과 대지저항 측정 시 각도와 거리를 정확하게 위치시켜 보조전극을 설치할 수 있는 접지저항 측정장치 및 측정방법을 제안한다. 정확한 접지저항 값을 선정할 수 있게 하기 위해 설치된 전극을 통해 접지저항 값뿐만 아니라, 대지저항률을 취득할 수 있어 유사지역에 전기시설물 설치 시에 유용한 자료로 활용할 수 있다. 또한 신뢰성 높은 데이터를 활용하고 현장의 대지구조를 분석하여 공사비용 뿐 아니라 접지설계에서 중요한 비중을 차지하는 대지에 대한 정밀한 분석으로 전위상승 등의 접지설비설계에서 많은 활용이 기대된다.

• 한국재난정보학회 논문집
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• 제17권4호
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• pp.684-693
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• 2021

연구목적: 아두이노를 이용하여 실시간 대지저항 데이터를 취득할 수 있는 스마트 대지저항 측정장치를 개발하여 낙뢰 등 이상전압으로부터 안전한 설비환경을 구축하는것에 목적이 있다. 연구방법: 본 논문은 아두이노와 전력선 통신(PLC) 체계를 갖춘 대지저항 취득 및 분석 시스템을 개발하여 설계모델과 적용사례를 연구하였다. 경남지역의 풍력발전 단지 내 일부 부지를 테스트 베드로 선정하여 신기술을 적용한 실시간 대지저항 데이터를 취득하였다. 전극배열은 웨너(Wenner) 4전극배열과 슐렘버거(Schlumberger) 전극배열을 혼용한 스마트 전극배열을 채택하였다. 연구결과: 본 기술의 특징은 첫 번째로 스마트 다 전극의 깊이를 각기 다르게 편성해 층간에 특이성을 가지는 지층 구조에도 취득 데이터의 오차범위를 축소하였다. 두 번째로 스마트 접지전극에서 취득한 대지저항 데이터의 정보를 사물인터넷으로 실시간 송·수신이 가능하도록 IT융합 기술을 적용하였다. 마지막으로 규칙적인 관리 체계를 구축하고 Server에 축적된 빅 데이터를 분석하여 다양한 요소들의 변화추이를 확인할 수 있으며, IT융합 환경에 최적의 접지 알고리즘과 접지시스템 설계 모델링이 가능하다. 결론: 본 기술은 4차 산업 시대에 근간이 되는 도시 기반시설에 낙뢰로 인한 서지(Surge)의 피해를 줄이고 최적화된 접지시스템 모델을 설계하여 사용자의 안전과 생명을 보호 할 것이다. 또한 순수 국산 기술력의 지적재산권을 확보하여 포스트 코로나 시대에 팬데믹으로 정체되어있는 우리산업의 일자리 창출과 활기를 불어넣는 효과도 기대된다.

• Smart Structures and Systems
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• 제16권4호
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• pp.743-758
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• 2015

This paper presents an advanced life cycle cost (LCC) analysis of a ground source heat pump (GSHP) system and suggests a smart operation mode with a thermal performance test (TPT) and an energy pile system constructed on the site of the Incheon International Airport (IIA). First, an economic analysis of the GSHP system was conducted for the second passenger terminal of the IIA considering actual influencing factors such as government support and the residual value of the equipment. The analysis results showed that the economic efficiency of the GSHP system could be increased owing to several influential factors. Second, a multiple regression analysis was conducted using different independent variables in order to analyze the influence indices with regard to the LCC results. Every independent index, in this case the initial construction cost, lifespan of the equipment, discount rate and the amount of price inflation can affect the LCC results. Third, a GSHP system using an energy pile was installed on the site of the construction laboratory institute of the IIA. TPTs of W-shape and spiral-coil-type GHEs were conducted in continuous and intermittent operation modes, respectively, prior to system operation of the energy pile. A cooling GSHP system in the energy pile was operated in both the continuous and intermittent modes, and the LCC was calculated. Furthermore, the smart operation mode and LCC were analyzed considering the application of a thermal storage tank.