• Journal of the Korea Society for Simulation
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• v.27 no.1
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• pp.15-24
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• 2018

High Level Architecture(HLA) for modeling and simulation is an international technical standard to achieve simulation interoperability and reusability. Building federation through the interworking of federates is being used in various fields and is being used in KR(Key Resolve), UFG(Ulchi-Freedom Guardian) as a representative in domestic military. Currently, United States Department of Defense emphasizes the HLA compliance test, which confirms the compliance of Federate by using HLA. However, due to the limitations of testing tools, an HLA compliance test of DoD is not able to perform some of the functional tests on HLA/RTI services such as federation storage/recovery services and also exclude inspection of exchange data between federates. To solve these problems, this paper proposes an HLA compliance testing system of ROK suitable for domestic situations. This will enable effective HLA compliance testing and improve interoperability between federates.

• TTA Journal
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• s.37
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• pp.32-48
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• 1995

최근에 복잡,다양해지는 정보통신환경에서의 정보통신기기간 상호운용성이 중요한 이슈로 부각되면서, 국내에서도 정보통신기기에 대한 국가권고표준의 준수 여부를 검증할 필요성이 폭넓게 인식되어 가고 있다. 본 고에서는 이러한 국가권고표준 적합인증의 전반적인 절차에 적용될 ''OSI 상호접속-적합성시험 방법론 및 체계'' 표준안에 대한 이해를 돕기 위하여, 본 표준안의 제정 배경과 주요 내용, 그리고 적합성시험 방법론과 시험지침을 설명한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.6
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• pp.526-532
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• 2015

In order to relieve limitation of flight operation under icing condition and verify its operation in adverse weather condition for Surion, military helicopter developed in Korea, airworthiness certification in icing condition is required. The process of Surion icing certification should be considered by implementation of four methods by step such as CFD analysis, simulated flight tests, artificial icing flight tests, and natural icing flight tests. For Surion icing flight tests, these are required 20~30 sorties and 20~23 hours in artificial icing condition; 20~30 sorties and 20~22 hours in natural icing condition. In addition, to proceed with efficient flight tests, it is necessary to implement artificial icing flight tests in LWC $0.5{\sim}1.0g/m^3;$ natural icing flight tests in less than LWC $0.5g/m^3$.

• Aerospace Engineering and Technology
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• v.11 no.2
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• pp.216-224
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• 2012

This study described about the procedure and method to type certification of KAS 23 civil aircraft that is developed in domestic. It is important to obtain type certification within defined period based on the proposed process and method to prove compliance through certification basis according to certification plan. This process referred to FAA Order 8110.4 C, "Type Certification" and domestic regulation and showed example of compliance check list(CCL) defining means of compliance(MOC). Also, proposed method to prove compliance according to means of compliance and classified item of test & evaluation.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2018.06a
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• pp.22-22
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• 2018

의료기기는 사용목적과 사용 시 인체에 미치는 잠재적 위해성의 정도에 따라 4개의 등급으로 분류하며, 두 가지 이상의 등급에 해당되는 제품의 경우에는 가장 높은 등급으로 분류하게 된다. 의료기기 품목허가를 위해서는 기술문서를 작성하여야 하며, 이를 위해서는 기술문서 심사를 신청하는 절차를 이해하여야 한다. 의료기기 기술문서란 의료기기의 성능과 안전성 등 품질에 관한 자료로서 해당 품목의 원자재, 구조, 사용목적, 사용방법, 작용원리, 사용 시 주의사항, 시험규격 등이 포함되는 문서를 말하며, '의료기기 허가 신청서'와 '첨부자료(임상시험자료 포함)'로 구성되어 있다. 의료기기 품목허가 시 제출되는 기술문서를 통하여 해당 의료기기의 안전성 및 성능이 충분히 입증되어야 하며, 인체 삽입되는 표면처리 임플란트를 포함한 인체 접촉 의료기기의 안전성의 경우 '의료기기의 생물학적 안전에 관한 공통 기준규격'에 따라 평가 후 제조 수입품목 허가를 진행해야 한다. 또한 성능의 경우는 해당 규격 또는 자사의 기준 및 시험방법에 따른 성능에 관한 자료, 물리 화학적 특성에 관한 자료를 통하여 평가되어야 하며, 기허가 인증된 제품에 한 번도 사용되지 않은 원재료 또는 적용부위 및 적용방법이 달라 안전성 및 유효성 확인이 필요한 경우 임상시험에 관한 자료가 요구될 수 있다. 본 발표에서는 이러한 인체 삽입용 표면처리 임플란트의 전반적인 인허가 절차에 대해서 안내하고자 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.4
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• pp.308-315
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• 2007

This study is performed to find out the climb performance of light airplane, Chang Gong-91, as a part of flight test to acquire the certification. Chang Gong-91 is a 5-passenger light aircraft of normal category with single reciprocating engine, and the first officially certified by Korean Ministry of Construction and Transportation in 1993. These flight test procedure and data for climb performance are used to get type certification. We have got maximum climb rate for operating altitude, best angle of climb speed, best rate of climb speed, and absolute ceiling of Chang Gong-91 using drag polar data reduction method from sawtooth climb flight data. Also we compare the form drag coefficient from the results of climb performance and Oswald's effectiveness coefficient to design values using lift-drag curve of light airplane.

• Journal of Advanced Navigation Technology
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• v.23 no.4
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• pp.281-288
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• 2019

A Flight test is an important process that must be performed to maintain airworthiness in the aircraft lifecycle, including aircraft development and certification. Flight test can be conducted for the purpose of demonstrating or verifying compliance with the applicable standard. Results of the flight test air accident analysis confirm that it is caused by a combination of various factors as well as aircraft. The International Civil Aviation Organization recommends the establishment and implementation of a safety management system to prevent aircraft accidents, but it does not reflect the specificity of the flight test. As such, advanced countries are providing separate criteria to assist stakeholder in conducting flight test safety management. This study investigates and analyzes relevant regulations of advanced countries, in accordance with the construction of a national flight performance test site in Korea, and proposes government-level guidelines to help stakeholders develop their flight test operation manuals. The guidelines discuss topics such as organizational composition, safety and risk management, flight operation, personnel management, and administrative issues.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.4
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• pp.91-99
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• 2005

Flight compatibility certification is performed to substantiate the compatibility between ALQ-X ECM pod and KF-16D/RF-4C aircraft. A certification plan for the ALQ-X flight compatibility is established. Similarity analysis, mass/inertia analysis, structural analysis/test, and ground vibration test/flutter analysis are made to support the safety of MIL-HDBK-1763 Test 250 (Captive compatibility flight profile). Aircraft flew along flight envelope boundary with representative ALQ-X configurations. Handling qualities are evaluated by comparing flight characteristics of the aircraft with and without ALQ-X. Structural integrity and endurance is evaluated using measured flight test data. Results of these flight tests showed that ALQ-X is compatible with KF-16D/RF-4C without altering the flight envelope which has originally been certified for ALQ-88 and ALQ-119 ECM pods. ALQ-X certification program made following technical achievements: Type III certification for foreign designed fighter, flutter analysis program development using GVT results, and utilization of MIL-STD-1553B data bus in flight test.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.198-200
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• 2017

An Auxiliary Power Unit (APU) is a small gas turbine engine that is mounted on an aircraft and serves to supply energy for ground and air starting of the main engine. APU also supplies emergency and auxiliary power for the aircraft. APU for aircraft is simple and compact in structure, but because it is mounted on manned aircraft, high reliability is required, so it must be proved its reliability through qualification procedure. The Korea Aerospace Research Institute and Hanwha Techwin successfully completed the design / analysis, fabrication, assembly, development test and certification test of APU for helicopter based on accumulated domestic R & D capability and experience from 2007 to 2012. In this paper, the development and certification process of auxiliary power unit for helicopter is summarized.

• Proceedings of the CALSEC Conference
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• 1997.11a
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• pp.237-261
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• 1997

◆ 국내의 CALS/EC 시스템 구축시 적용할 표준 및 제품에 대한 기준 및 인증절차 제시 ⇒ CALS/EC 구현제품과 데이타 표준에 대한 품질향상 및 국제 신뢰성 확보 ⇒ 국내 CALS/EC 시스템 구축의 가속화와 국제 경쟁력 강화(중략)