• 한국항공운항학회:학술대회논문집
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• 2016.05a
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• pp.228-232
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• 2016

유/무인기가 통합되어 운용되는 환경을 고려한 시뮬레이션 시스템 설계 방안을 제시하였다. 기존의 관제 공역 내의 유인기를 대상으로 하는 항공 교통 시뮬레이션 시스템의 기능과 무인기 시스템의 기본적인 기능을 고려하였으며, 이를 기반으로 유/무인기 복합 운용의 새로운 개념을 적용하여 모의할 수 있는 시뮬레이션 환경을 구성하였다. 모의 환경의 확장성을 고려하여, 무인기는 관제 공역에 진입하여 유인기와 복합 운용되는 무인항공기 시스템과 비관제 영역에서 운용되는 소형 무인비행장치로 구분하여 구성하였다. 시뮬레이션 시스템을 구현하기 위한 운용 개념에 대해 서술하였으며, 이를 기반으로 필요로 하는 주요 기능 요소들을 구성하고 각 요소에서 고려되어야 하는 주요 요구 사항을 제시하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.5
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• pp.423-430
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• 2016

Recently, manned and unmanned aerial vehicles are faced with problems such as collision detection and avoidance, link-loss for integrated operations in NAS. Hence, on the basis of the performance data of EUROCONTROL's BADA and NASA, an environment was developed to simultaneously handle simulations of integrated operations of MAVs and UAVs along with ATC/ATM simulations, and dynamic modeling was then carried out. To validate the developed model, simulations were performed on a 6-DOF model by its segments and the results were compared to the RMSE results.

• Journal of Aerospace System Engineering
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• v.13 no.6
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• pp.36-42
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• 2019

This research illustrates how the simulation environment for operating the simultaneous man/unmanned aerial vehicle teaming is constructed. X-Plane program, HILS for the ducted fan aircraft (unmanned) and CTLS (manned aircraft) with communication devices are interfaced to simulate the basic co-operational flight. The X-plane and HILS can allow operators to experience the maned and unmanned aircraft operation in the airspace on the ground in turn they can perform various simulated missions in advance before the actual flight. For the test purpose, the data link between man/unmanned aircraft and ground control station is examined using C Band and UHF radio channels by the manned aircraft.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.8
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• pp.662-670
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• 2017

This paper proposes an optimization-based procedure to determine the parameters of the Apollo guidance law for Korean lunar lander mission. A lunar landing mission is formulated as a trajectory optimization problem to minimize the fuel consumption and the reference trajectory for the lander is obtained by solving the problem in the pre-flight phase. Some parameters of the Apollo guidance, which are coefficients of the polynomial used to define the guidance command, are selected based on the reference trajectory obtained in the pre-flight phase. A case study for the landing guidance of Korean lunar lander mission using the proposed procedure is conducted to demonstrate its effectiveness.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.10
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• pp.820-826
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• 2013

In this paper, a compact and wideband CLAS(Conformal Load bearing Antenna Structure) was studied using smart skin technique. In order to satisfy the electrical performance of the CLAS antenna, the proposed CLAS antenna is composed of conductive mesh, face-sheet, radiator, honeycomb, housing. Especially, radiator is composed of composite magneto-dielectric material and radiating element etched on the PCB (Printed Circuit Board). The radiating element is inserted into the composite magneto-dielectric material and has sloted Folded LP(Log Periodic) structure. By fabricated composite magneto-dielectric, the resonance frequency is decreased and the impedance matching characteristics is improved. We verified that the antenna has wideband characteristics and compact size using the antenna test results.

• 한국항공운항학회:학술대회논문집
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• 2007.12a
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• pp.57-62
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• 2007

• 한국항공운항학회:학술대회논문집
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• 2005.11a
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• pp.209-212
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• 2005

• The Korean Journal of Air & Space Law and Policy
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• v.13
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• pp.167-206
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• 2001

• Proceedings of the Korean Society of Computer Information Conference
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• 2023.01a
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• pp.453-454
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• 2023

4차산업 혁명의 대표 영역인 인공지능은 과학기술뿐 아니라 사회, 경제, 문화 등 우리 사회의 전 분야에 적용되어가고 있다. 이것은 교육기관에서 인공지능 관련 컴퓨터 전공자만이 아닌 여러 전공 각 분야의 전공자 또한 인공지능 교육을 받아야 함을 의미하는 것이다. 이에 따라 전 분야에 걸친 A·I융합 인재의 양성이 관심사항이 되고 있다. 본 논문에서는 항공정비사 양성을 위한 국토교통부 전문교육기관 지정기준에 제시된 교육과목 및 내용에 소프트웨어 교육을 위해 시스템 제어에 관한 이론/실습교육의 추가를 제안하였다. 제안한 교육내용은 항공정비 분야에서의 A·I융합 인재양성에 한 방안이 될 것이라 기대한다.

• Journal of the Korean Society of Marine Environment & Safety
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• v.20 no.6
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• pp.781-787
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• 2014

The dimensionless extinction constants of particulate matter for F-76 diesel and JP-8 aviation fuels were measured at both 633 nm and 853 nm in the transmission cell where the simultaneous gravimetric measurement of PM concentration is compared to the light extinction measurement. For the F-76 diesel PM, the average value of the dimensionless extinction constants at 633 nm was 8.8 whereas that of the dimensionless extinction constants for JP-8 was 9.8 at the same wavelength. As the wavelength is increased to 853 nm, the average value for the F-76 diesel was reduced to 8.2 whereas that for JP-8 was decreased to 8.9.