• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.42 no.9
• /
• pp.731-738
• /
• 2014

The mission of UAV has been expanded from a land to an ocean based on an enhancement of its technologies. Korea Aerospace Research Institute (KARI) also tries to expand the mission of tilt rotor UAV to an ocean, in which the shipboard landing of UAV is required. However the environment of an oceanic operation is severer than that of land due to salty, fogy, and windy condition. The landing point for automatic landing is not fixed due to movement of shipboard in roll, pitch, and heave. It makes the oceanic operation and landing of UAV difficult. In order to conduct an oceanic operation of tilt rotor UAV, this paper presents that the sea wave modeling according to the sea state is conducted and the shipboard landing of tilt rotor UAV under the sea wave is tested and evaluated through the flight simulator for UAV.

• Proceedings of the Korea Water Resources Association Conference
• /
• 2011.05a
• /
• pp.92-92
• /
• 2011

수자원장기종합계획(2006)에 따르면, 우리나라는 물부족이 예상이 되고 있고, 이러한 물부족 현상은 기후변화의 영향으로 더욱 악화될 것으로 예상된다. 기후변화에 따른 물부족에 대응하기 위해서는 현행 지표수 및 지하수(Blue Water) 위주의 수자원관리와 더불어 그전에는 수자원으로 인식되지 않았던 토양수(Green Water)를 새로운 개념의 수자원으로 인식하는 것이 필요하다. 토양수는 현재 물사용량 중에서 가장 많은 비중을 차지하는 농업용수 부분에 효율적으로 활용하면, 지표수나 지하수와 같은 수자원을 대체하는 효과가 있다. 기후변화에 따른 물부족에 대응한 토양수의 효율적 활용을 위해서는, 과거 뿐아니라 미래의 지역별 시기별 토양수 공간분포특성을 분석하는 것이 선행되어야 한다. 그러므로 본 연구에서는 토양수의 분석을 통한 미래 물부족 해결에 도움이 될 새로운 수자원 관리의 기틀을 마련하기 위해 토양수 분포특성분석모델을 개발하고, 이를 활용해 과거 및 미래의 토양수의 공간분포특성을 분석한다. 토양수 분포특성분석모델은 선행 5일간의 일 강우데이터 값을 표준선행강우지표(Normalized Antecedent Precipitation Index)에 적용하여 일 단위 토양수 상태(Wet, Average, Dry condition)를 계산하는 모델이다. 과거 토양수 분석에는 인공위성 강우데이터(Tropical Rainfall Measuring Mission 3B42)를, 미래 토양수 분석을 위해서는 기상청에서 제공하는 국가표준 기후변화 시나리오(A1B)를 각각 사용하여, 과거 데이터는 27km의 격자로, 미래는 25km 격자크기로 한반도 전체의 일 단위 토양수 상태를 계산했다. 계산된 토양수 결과를 활용해 연 월별 그리고 토양수를 쓸 수 있는 시기, 즉 식물이 자라는 시기(4-9월)의 특성을 분석했다. 이를 통해 향후 기후변화에 따른 물부족 대응 토양수 수자원 활용방안에 도움이 될 것으로 예상된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.50 no.3
• /
• pp.173-180
• /
• 2022

The operation and transportation environment for an unmanned aerial vehicle will be completely different from those for the conventional air and ground transportation. The requirement for a traffic management system for its safe operation has been emerging. Accordingly, investigation is being conducted to analyze the danger that unmanned aerial vehicle may encounter during the flight and to provide the countermeasure by the simulation. When the drones operate in an urban environment, they may be affected by the wind around the building. Thus it is essential to predict the influence of the gust and analyze the resulting risk. In this paper, a method for evaluating the safety for a flight mission under the gust is suggested. By using the precise 6-degree-of-freedom flight simulation that is capable of simulating the gust condition, possible deviation from the pre-planned flight path in terms of the attitude orientation will be predicted. A method of quantifying the probability of the flight mission failure will also be presented.

• 한국전산유체공학회:학술대회논문집
• /
• 2009.04a
• /
• pp.81-85
• /
• 2009

In this paper, the aerodynamic shape of air intake was investigated for the efficient cooling of electronic equipments in aircraft pod. As a first step, ESDU method was applied for the basic shape design of air intake considering the operational environments. The second step was to confirm the performance on design point, so the internal flow field of air intake was analyzed using a commercial Navier-Stokes code(FLUENT). And also the aerodynamic characteristics of internal flow at off-design condition was investigated with the variations of airflow rate. The results show that the air intake meets the requirement of target performance under the mission environments.

• Proceedings of the KSME Conference
• /
• 2007.05a
• /
• pp.1595-1600
• /
• 2007

It is necessary a simple helicopter design and performance analysis program for a stage of helicopter conceptual design. To meet that needs, we have developed a program which is simply used to estimate helicopter configuration and performance. The program developed by this study is composed of Requirement, Mission profile Analysis, Size, Aerodynamic, Trim, Propulsion, Weight, and Performance modules, and each modules carry out operations for a given flight condition. In this study, we validate this analysis program in 9,500 1bs and 22,000 1bs helicopters and estimate design configuration and performance of 16,000 1b helicopter. And We can use this program to optimization process for Helicopter MDO framework.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2002.11b
• /
• pp.250-254
• /
• 2002

It is conducted to analyze vibration loads on KSR-III(KSR: Korea Sounding Rocket) and its major segments during their ground transportation and various handling process. These loads may be different from the real flight environment. Inadequate assessment of these loads can cause not only local damages on the rocket system but also the critical problem like flight mission failure. Therefore, transportation and handling loads must be considered during design and attenuated to ensure that the rocket structural damage does not occur. This work is concerned with the generation of criteria and prediction of transportation and handling loads for KSR-III. The results show that the shipping container is well designed to satisfy the design requirements. The maximum vibration level recorded during whole transportation and handling for KSR-III is less than 2g, the criteria of KSR-III movement condition.

• Journal of the Korean Society for Aviation and Aeronautics
• /
• v.18 no.4
• /
• pp.1-8
• /
• 2010

In the aerospace field, the study on a morphing-wing is in progress to improve flight performance and perform multi flight mission. There are many concepts of morphing-wing such as camber-change, wing-twist, variable-span, and so on. In this study, the aerodynamic characteristics and flight control of an air vehicle with a variable-span morphing wing (VSMW) have been investigated. VSMW with symmetric span control(SSC) can increase cruising range of aircraft by reducing drag in various flight condition. VSMW with anti-symmetric span control(ASSC) can be used in the roll control of an aircraft. The flight control about pure rolling dynamic system and full dynamic system have been performed about the cruise missile.

• Korean Security Journal
• /
• no.7
• /
• pp.155-189
• /
• 2004

The mission of the police as described by law is to guard the life, body and property of all citizens. Such duties should be accurately performed based on legal and democratic procedures because the works of the police are directively influencing the overall lives of the citizens by restricting their freedom. We are frequently watching the traffic police on the street or road. Traffic policing aims to reduce crime and the opportunities for criminal activity in relation to the use of roads, that is to improve road user behavior in order to reduce accidents. The characteristics of traffic accident change is not similar in each traffic condition. The purpose of this study is to analysis a type characteristics of traffic accident change, such as number of deaths and wounded persons by the time, the vehicle, the type the road, the age group. Based on the characteristics of traffic accident change, traffic accident countermeasures are proposed, in which some variable of traffic policies such as traffic facilities, traffic regulation, and traffic safety education.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2009.05a
• /
• pp.385-390
• /
• 2009

The gas turbine engine structures usually are placed on high thermal mechanical stress condition. For general low cycle fatigue evaluation, simple fatigue criterion based on critical plane approach is developed. LCF life of turbine wheel is evaluated with this criterion and process contrived together.

• Aerospace Engineering and Technology
• /
• v.2 no.1
• /
• pp.63-72
• /
• 2003

On the basis of sensor types, satellites can be classified by two types, which are optical observation satellite and radar observation satellite. A satellite type is selected according to the specific mission. Optical observation satellite is more appropriate for getting high geometric resolution images and radar observation satellite is more appropriate for getting images independent of weather condition the more a demand of satellite increases, the more an importance of information increases. Therefore, development trend and state of earth observation satellite are surveyed and described in this paper. In the future, domestic development of satellites will be planned considering trend of satellite technologies.