• Transactions on Control, Automation and Systems Engineering
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• 제4권2호
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• pp.114-123
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• 2002

Called VISTA (Variable-stability In-flight Simulator Test Aircraft), the one-of-a-kind NF-l6D has a simulation system that can mimic several aircraft. Though housed in an F-l6 Fighting Falcon airframe, VISTA can also act like the F-15 Eagle or the Navy's F-14 Tomcat. More importantly, such flexibility allows for improved training and consolidation of some sorties. Consequently USAF Test Pilot School students will have an opportunity to learn how to test future integrated cockpits. In this paper we will use the multiple model adaptive estimation (MMAE) and the multiple model adaptive controller (MMAC) techniques to model the aircraft's flight control system containing the longitudinal and lateral-directional axes. Single and dual actuator and sensor failures will also be included in the simulation. White Gaussian noise will be included to simulate the effects of atmospheric disturbances.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2008년도 추계 학술발표회
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• pp.1007-1013
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• 2008

In this study, a series of scaled model test were carried out in order to find factors that influence the ultimate load of underreamed anchors. Model anchors were made of arcril and 3cm in diameter. Series of tests were performed with various conditions such as density of soil, diameter of bulb, and number of bulb. Type of soil was Jumunjin sand and relative density varied 40%, 60%, 80%.

• 한국정밀공학회지
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• 제18권3호
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• pp.143-151
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• 2001

Machine tool errors have to be characterized and predicted to improve machine tool accuracy. A real-time error compensation system has been developed based on volumetric error synthesis model which is composed of machine tool errors. This paper deals with new algorithm about verification of machine tool errors. This new algorithm uses a simplified volumetric error synthesis model. This simplified model is constructed with only main components among the error components of the machine. The main error components are analyzed by ball bar test of hemispherical helix. The novel measurement method using ball bar system has many advantages which are more efficient, easier to use than conventional measurement system.

• 대한화장품학회지
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• 제17권1호
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• pp.64-80
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• 1991

The SKINTEX Method is based on a two-compartment physico-chemical model which includes a Biomembrane Barrier in compartment one and an organized macromolecular matrix in compartment two. Test samples absorb onto or permeate through the keratin/collagen Biomembrane Barrier and then can interact with the organized macromolecular matrix. Changes in the integrity of the barrier release a dye indicator: Changes in the matrix can alter its transparency. The sum of these two responses is read spectrophotometrically at 470nm. An early investigation of 950 chemicals and formulations in the SKINTEX System produced results which were 89% concordance to in vivo Draize dermal irritation results obtained with 24-hour occluded application of test samples with-out abrasion and standard scoring. Alkaline materials were analyzed in a specialized SKINTEX AMA Protocol. In this early study, the model did not distinguish nonirritant test materials and formulation with PDII(Primary Dermal Irritation Index)in the range from 0 to 1.2, A High Sensitivity Assay Protocol(HSA)was developed to amplify the changes in both compartments of this model and provide more accurate calibration of these changes. A study of 60 low irritation test samples including cosmetics, household products, chemicals and petro-chemicals distinguished nonirritants with PDII $\leq$ 0.7 for 26 of 30 nonirritants. A second protocol was developed to evaluate the SKINTEX model predictability with respect to human irritation. The Human Response Assay (HRA )has been optimized based on differences in penetration and irritation responses in humans and rabbits. An additional 32 test materials with different mechanisms and degrees of dermal toxicity were evaluated by the HRA. These in vitro results were 86% concordant to human patch test results. In order to further evaluate this model, a Standard Chemical Labelling (SCL) Protocol was developed to optimize this system to predict Draize dermal irritation results after a 4-hour application of the test material. In a study of 52 chemicals including acids, bases, solvents, salts, surfactants and preservatives, the SCL results demonstrated 85% concordance to Draize results for a 4-hour application of test samples on non-abraded rabbit skin. The SKINTEX System, including three specialized protocols, provided results which demonstrated good correlation to the endpoint of dermal irritation in man and rabbits at different application times.

• International Journal of Reliability and Applications
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• 제18권2호
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• pp.45-63
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• 2017

In this paper, we have formulated optimum Accelerated Life Test (ALT) plan for a parallel system with two independent components using masked data with ramp-stress loading scheme and Type-I censoring. Consider a system of two independent and non-identical components connected in parallel. Such a system fails whenever all of its components has failed. The exact component that causes the system to fail is often unknown due to cost and time constraint. For each parallel system at test, we observe its system's failure time and a set of component that includes the component actually causing the system to fail. The stress-life relationship is modelled using inverse power law, and cumulative exposure model is assumed to model the effect of changing stress. The optimal plan consists in finding out the optimum stress rate using D-optimality criterion. The method developed has been explained using a numerical example and sensitivity analysis carried out.

• 한국항해항만학회지
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• 제33권9호
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• pp.603-608
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• 2009

In this paper, a 3m-class free running model ship will be introduced with its manoeuvring performance experiments. The results of turning circle test and zig-zag test will be explained. The developed system are equipped with GPS, main control computer, wireless LAN, IMU (Inertial Measurement Unit), self-propulsion propeller and driving rudder. Its motion can be controlled by RC (Radio Control) and wireless LAN from land based center. Automatic navigation is also available by pre-programmed algorithm. The trajectory of navigation can be acquired by GPS and it provides us with important data for ship's motion control experiments. The results of manoeuvring performance experiment have shown that the developed free running model ship can be used to verify the test of turning circle and zig-zag. For next step, other experimental researches such as ship collision avoidance system and automatic berthing can be considered in the future.

• Journal of Mechanical Science and Technology
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• 제15권2호
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• pp.152-159
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• 2001

In this paper it is intended to set-up a sound model of the 60,000rpm 100kW prototype APU gas turbine rotor-bearing system, and particularly to investigate the influences of the tie shaft on the rotordynamic characteristics of the entire APU gas turbine rotor-bearing system, employing the dual shaft model. Firstly, a mock-up APU rotor has been constructed to test and verify the model. Analytical natural frequency results have agreed with the corresponding modal test ones to within 5% difference. Then, the rotordynamic characteristics of the prototype APU rotorbearing system have been investigated. Natural vibration and unbalance response analyses results have shown that the inner tie shaft resonance can cause high enough vibration of the outer main rotor shaft. This could be a concern as the rotor journals operate on very thin air film at high speed. It is concluded as a conservative design practice that the inner tie shaft should be explicitly modeled in the rotordynamic analysis of the APU rotor-bearing system.

• 한국지반공학회논문집
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• 제23권7호
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• pp.27-36
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• 2007

프리스트레스트 띠장을 적용한 흙막이 시스템의 안정성을 평가하고 거동 특성을 규명하기 위하여 모형 시험이 수행되었다. 본 흙막이 시스템의 모형 시험을 위해 현장 규모의 프리스트레스트 띠장을 적용한 흙막이 시스템에 대한 차원 해석이 수행되었다. 본 논문에는 새로운 흙막이 시스템에 대한 차원 해석의 절차 및 방법이 제시되어 있다. 차원 해석 결과로부터 모형 규모의 프리스트레스트 띠장을 적용한 흙막이 시스템을 구현하였다. 모형 시험 중 새로운 흙막이 시스템 부재에 대한 계측을 수행하여 흙막이 벽체 배면의 토압 거동, 프리스트레스트 띠장의 변형 거동, 띠장 시스템 부재의 힘 거동과 버팀보의 힘 거동을 파악하였다. 모형 시험 결과는 프리스트레스트 띠장 시스템 부재의 설계 결과와 비교 평가되었다.

• 동력기계공학회지
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• 제4권2호
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• pp.71-76
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• 2000

It is well known that finite element analysis often has the inaccuracy when they are in conflict with test results. Model updating is concerned with the correction of analytical model by processing records of response from test results. This paper introduce a model updating technique using the frequency response function data. The measurement data is able to be used directly in the FRF sensitivity method because it is not necessary to identify. When a damping model is updated, it is necessary for the sensitivity matrix to be divided Into the complex part and real part. As an applying model, a cantilever and a rotor system are used. Specially the machined clearance($C_p$) of the journal bearing is updated.

• 한국산학기술학회논문지
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• 제20권1호
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• pp.268-277
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• 2019

유도무기 비행시험 시스템은 비행시험 중 여러 가지 상태를 실시간으로 감시하고 비상상황 발생 시 안전조치를 수행할 수 있어야 한다. 점차 복잡화, 광역화되고 있는 비행시험의 환경 변화 속에서 시험안전 확보의 중요성이 더욱 증대되고 있다. 또한 국내외 정세 변화와 전시작전권 전환 등으로 인하여 다수의 유도무기체계가 동시에 개발되어야 하고 동시에 연구개발 및 시험평가 기간단축을 통한 조기 전략화 및 예산절감도 요구되는 상황이다. 이에 따라 국내의 부족한 시험장 자원 여건 하에서 비행시험 시 발생되는 위험은 증가하고 있으며 시험안전 확보를 위한 대책 마련이 시급한 실정이다. 이러한 요구에 부응하기 위해서 연구개발 초기 단계에서부터 비행시험 시스템의 문제를 식별하고 대처방안을 마련할 수 있도록 모델기반 비행시험 시스템 개발을 본 연구의 목표로 설정하였다. 구체적으로 유도무기 비행시험의 설계 및 검증 방법을 제안하였다. 제안된 방법은 선진 시험평가기관에서 연구하고 있는 Agile 방식의 Shift Left 시험평가 방법론과 항공우주분야에서의 시스템 참조모델을 활용하였다. 연구개발 단계에서 유도무기체계와 동시에 설계를 진행하고 비행시험 요구사항에 대한 상호 간의 결함을 조기에 식별하여 수정함으로써 시험평가 단계에서 수행하는 비행시험 시 발생될 위험을 완화할 수 있다. 또한 항공우주분야에서 복잡한 시스템을 통합하고 검증하는 데 적용하고 있는 참조모델을 기반으로 시스템 모델링 표준 언어인 SysML을 활용하여 모델기반 비행시험 시스템을 구현함으로써 다수의 유도무기 비행시험 설계에 적용할 수 있는 확장성을 갖고 있으며, 시뮬레이션 분석을 통해 비행시험에서 발생하는 문제를 조기에 식별하고 조치함으로써 시험평가 기간의 지연을 방지할 수 있다.