• 대한인간공학회지
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• 제16권1호
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• pp.97-105
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• 1997

An aircraft simulator for ergonomics testing and pilot training was developed from the joint work Agency for Defense Development(ADD) and Daewoo Heavy Industry, LTD, in Korea at first time. It is basically to satisfy the requirements established by FAA-AC-120-40C ( 1995-JAN-26). The aircraft simulator will be used mainly for ergonomics testing and pilot training for basic trainer on ADD and Korea Air Force in near futrue. This simulator reproduces faithfully the cockpit and flight characteristics of the KTX-1 aircraft. It is one of the latest full flight simulators that have the CGI(computer graphic image) visual system and six degree of freedom motions system. Development efforts focused on user-oriented design approach for ergonomics testing and flight training of pilots. Main characteristics of each subsystem are described such as cockpit, instruments, control loading system, motion system, visual system, aural system, instructor operation station and aircraft simulation softwear.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.718-723
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• 2003

The number of jet aircraft is increasing. The aircraft noise making people near airports nervous have become a serious social problem. The aircraft noise can be classified into two groups; noise being generated at take-off or landing and noise form run-up test on the ground. In this paper, we consider the aircraft noise from run-up test on the pound and we suggest the noise suppression system.

• 한국항공운항학회지
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• 제23권1호
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• pp.1-7
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• 2015

The aircraft maintenance demands a lot of aviation mechanics in urgent according to the high season and low season in seasonal demand adjusted, unplanned maintenance work such as AD (airworthiness directives) and troubleshooting of aircraft system fault. The advent of Super-Large Aircraft such as A380 with aircraft materials, power plant and avionics systems which were not in previous models must be expected to increase the complexity of the aircraft maintenance system. This study is intended to propose the development plan for formation of positive flexibility culture in aircraft maintenance organization through the review of previous research on flexibility culture of organization and through empirical research for bureaucratic and poor factors by the evaluation of flexibility culture level of domestic aircraft maintenance organization.

• Smart Structures and Systems
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• 제1권2호
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• pp.159-184
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• 2005

The paper intends to summarize some guidelines for future smart structure system application in military aircraft. This preview of system integration is based upon a review on approximately one and a half decades of application oriented aerospace related smart structures research. Achievements in the area of structural health monitoring, adaptive shape, adaptive load bearing devices and active vibration control have been reached, potentials have been identified, several feasibility studies have been performed and some smart technologies have been already implemented. However the realization of anticipated visions and previously initial timescales announced have been rather too optimistic. The current development shall be based on a more realistic basis including more emphasis on fundamental aircraft strength, stiffness, static and dynamic load and stability requirements of aircraft and interdisciplinary integration requirements and improvements of integrated actors, actuator systems and control systems including micro controllers.

• International Journal of Aerospace System Engineering
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• 제3권2호
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• pp.1-8
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• 2016

The improvements in high performance and agility of modern fighter aircraft have led to improvements in survivability as well. Related to these performance increases are rapid response and adequate deflection of the control surfaces. Most control surface failures result from the failure of the actuator. Therefore, the failure and behavior of the actuators are essential to both combat aircraft survivability and maneuverability. In this study, we investigate the effects of flaperon actuator failure on flight maneuvers of a supersonic aircraft. The flight maneuvers were analyzed using six degrees of freedom (6DOF) simulations. This research will contribute to improvements in the reconfiguration of control surfaces and control allocation in flight control algorithms. This paper compares the results of these 6DOF simulations with the horizontal tail actuator failures analyzed previously.

• 산업경영시스템학회지
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• 제24권65호
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• pp.89-102
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• 2001

In this paper, the aircraft route scheduling consists of two steps; the pairing generation and the aircraft assignment. The pairing generation is heuristic approach how flights construct pairings from and to the main base. The aircraft resource assignment which is to establish a aircraft route schedule is constructed by constraint satisfaction problem technique. ILOG solver and schedule is used to solve this problem. In addition, a aircraft route reschedule process against departure-arrival delay or aircraft maintenance schedule change is added by partial constraints satisfaction problem technique. Also, Gantt chart made by ILOG views is used to show aircraft route schedule results more easily.

• 항공우주정책ㆍ법학회지
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• 제33권1호
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• pp.175-204
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• 2018

최근 항공레저사업이 법제화되고 관련된 산업이 제도권 내에서 활성화 기반을 갖추어 경량항공기의 도입과 운영이 늘어나고 있다. 2014년 개정된 항공법에서는 항공레저스포스사업이 영리행위를 위해 사업등록을 의무화하여 법적 제도권하에서 항공기체와 항공사업을 관리할 수 있도록 하였다. 그러나 경량항공기 안전문제에 있어서는 규정을 위반하여 비행하거나, 운영자의 안전의식 부족 및 능력 부족 등이 자주 언급되고 있으며, 개인 운영자들의 경우, 안전관리 미흡과 정비 불량 등 경량항공기의 사고위험이 상존하고 있다. 현재 우리나라에서는 경량항공기 정비는 관련 법규에 따라 항공정비사가 담당하고 있으나 자격과 전문성을 갖추었다고 보기는 어렵다. 항공정비사 제도상에 경량항공기 정비 업무를 담당하는 것이 법적인 문제가 되는 것은 아니다. 다만, 항공기, 경량항공기, 초경량비행장치를 구분하고 정비업무에서 포괄적으로 담당하도록 하고 있어 신뢰성과 적정성의 문제는 지속적으로 제기되고 있다. 즉, 경량항공기에 대한 법적, 제도적 체계를 분리하고 있음에도 많은 부분을 항공기 법조항에 준용규정 하고 있으며, 경량항공기 정비업무 역시 현 항공기 정비체계를 따르고 있는 것이다. 일반항공(General Aviation)이 발달한 미국, 유럽, 호주 등에서는 경량항공기 정비와 관련한 법적 제도적인 장치가 도입되었고, 전문적인 정비업무를 경량항공기 정비사 제도권에서 다루고 있다. 국내외 법령의 분석 결과 경량항공기 정비자격제도에 대한 도입이 필요하다. 미국, 유럽, 호주 등 일반항공 선진국에서는 경량항공기 정비사 제도를 두고 안전관리를 수행하고 있다. 이는 새로운 경량항공기 운영 환경 변화에 대처하기 위한 것이다. 본 연구에서는 단순히 경량항공기 정비사 제도에 대한 필요성만을 제시한 것은 아니다. 법적 체계의 관점에서도 제도의 보완이 필요한 부분인 것은 관련 법령의 검토 결과 나타났다. 해외 사례와의 비교에서도 도입의 필요성이 제기되는 것도 사실이다. 이러한 결과를 바탕으로 경량항공기 정비사 제도에 도입의 필요성은 있으며, 어떠한 방법으로 개선해 가는 것이 적절한지에 대한 방안을 제시해 보았다.

• Journal of Positioning, Navigation, and Timing
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• 제1권1호
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• pp.45-49
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• 2012

The flight performance evaluation of navigation system is very significant because the reliability of navigation data directly affect the safety of aircraft. Especially, the high-level navigation system such as DGPS/INS, need more precise flight performance evaluation method. The performance analysis is evaluated by comparing between the navigation system in aircraft and reference trajectory which is more precise than navigation system in aircraft. In order to verify DGPS/INS performance of m-level, the GPS receiver, which is capable post-processed Carrier-phase Differential GPS(CDGPS) method of cm-level, have to be used as reference system. The DGPS/INS is estimated the Center of Gravity (CG) point of aircraft to offer precise performance while the reference system is output the position of GPS antenna which is mounted on the outside of aircraft. Therefore, in order to more precise performance evaluation, it needs to compensate the lever arm and coordinates transformation. This paper use quaternion and Direct Cosine Matrix(DCM) methods as coordinate transformation matrix in lever arm compensation of CDGPS reference trajectory. And it compares NED errors of DCM and quaternion transformation in lever arm of reference trajectory via DGPS/INS result.

• 한국항공우주학회지
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• 제41권4호
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• pp.314-318
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• 2013

국내 최초로 개발되는 공대지 유도키트에 대하여 미국의 MIL-HDBK 및 STANDARD를 준용한 시험을 성공적으로 수행하였다. 각종 지상시험을 통하여 유도키트의 작동 성능과 내구성을 검증하였으며, 유도키트를 일반목적폭탄에 장착한 활공탄으로 비행시험을 수행하여 중거리 활공비행성능 및 정확도가 매우 양호함을 확인하였다.

• 항공우주시스템공학회지
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• 제2권4호
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• pp.13-18
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• 2008

Airworthiness is a term used to dictate whether an aircraft is worthy of safe flight. It is illegal in most countries to fly an aircraft without first obtaining an airworthiness certificate from the responsible government agency. For developing an aircraft, the design modifications and upgrades are considered a high financial risk proposal for most Program Managers(PMs). However Design-to-Certification Integrated System can be a great help in achieving a good design solution in an acceptable amount of time and flight test. In this paper, we present a method to construct database for the Development of Design-to-Certification Integrated System. By using this database, the human designer could manage and find the regulation and requirements related with his concern effectively.