• Journal of Aerospace System Engineering
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• v.16 no.3
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• pp.52-62
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• 2022

In the SORA methodology developed for the operational risk assessment of a specific category of operation of a UAS, the ground and the air risk levels are determined, and a SAIL indicating the level of assurance and integrity for the corresponding risk is assigned, and accordingly, the operational safety level for the proposed operation. Objectives should be demonstrated at an appropriate level of robustness. Because of the nature of the specific category of operation, people on the ground are the first risk subjects to be considered. The resulting ground risk class plays an important role in the allocation of SAIL. In this paper, the impact on SAIL and OSO according to the final risk level and the reduction of the level through the determination of the ground risk level and the application of mitigation measures among risk assessments for specific categories of UAV operation was investigated.

• The Journal of Aerospace Industry
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• s.69
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• pp.1-27
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• 2007

항공우주산업은 생산유발효과가 높고 고용창출도 높을 뿐만 아니라 부가가치산업이나, 대규모적 투자에 따른 투자 위험과 기술적 위험이 높아 정부차원에서의 개입이 불가피한 산업으로 인식된다. 최근 항공우주산업에 대한 정부의 지원 형태는 클러스터 조성, 지방세 감면, 토지 임대를 통한 기업지원 등 과거에 비해 더욱 다양한 형태로 발전되고 있다. 이와 같은 정부지원 형태의 다양성은 기존의 전통적 방식에 의한 지원으로는 글로벌 경쟁이 치열해지는 국제경쟁에서 경쟁력 우위를 유지하기 어렵다는 것을 반증하는 것이라고 할 수 있다. 특히 기존의 산업 중심의 정부지원 전략에서 기업중심의 정부지원 전략으로의 선회 경향은 산업의 주체는 기업이기 때문에 기업의 전체적 역량에 의한 경쟁우위가 글로벌 경쟁에서 보다 중요하다는 점을 시사하고 있다. 경남의 항공우주산업 클러스터 조성 여건은 인프라 구축면에서 여타 지역에 비해 매우 우수한 하부 기반을 구축하고 있어 클러스터 구축에 따른 효율성과 국제경쟁력 확보 가능성이 높다고 할 수 있다. 먼저, 클러스터 구축의 핵심이 되는 핵심선도기업인 KAI가 15년 전부터 대상지역에서 생산활동 중이며, 교육 및 훈련 기능도 비교적 풍부할 뿐만 아니라 공항도 인접해 있어 신속한 물류 및 정보공유, 해외시장과의 접근성이 높다고 할 수 있다. 결론적으로 볼 때, 경남지역의 항공우주산업 클러스터 구축의 타당성은 높다고 할 수 있다. 특히 현재의 항공우주산업 발전 단계상으로 볼 때, 부품산업의 발전이 긴요한 과제이므로 동 클러스터는 항공우주 부품 수출중심의 핵심 거점 클러스터로의 조성할 필요성이 높다고 할 수 있다. 이와 같은 클러스터 조성에 따른 경남 항공우주 클러스터의 운영체계는 “항공우주산업 혁신 클러스터 추진단”을 중심으로 입주 업체, 항공우주 수출 지원단, 관련 R&D 기관 및 교육기관 등이 긴밀하게 연계 되어 운영되어야 할 것이다. 이외에도 중앙정부와의 협의 및 관련 단체들과의 연계를 통해 클러스터의 효율성과 경쟁력 제고를 위한 활동을 적극 추진해야 할 것이다.

• Aerospace Engineering and Technology
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• v.7 no.2
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• pp.123-130
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• 2008

Flight safety analysis, which includes risk estimation for the various abnormal flight modes in addition to normal flight, has to be performed necessarily to guarantee launch safety for the operation of space launch vehicles. For this purpose, a dedicated system has been developed such that all the necessary repetitive computations, result reports, and graphical presentations can be performed inside a single system for user convenience. In addition, the developed system is capable of representing computed results on a three dimensional Earth for the realistic presentation. The developed Flight Safety Analysis System will be employed for the launch operation of Korea Satellite Launch Vehicle-I.

• Journal of Advanced Navigation Technology
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• v.24 no.6
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• pp.500-507
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• 2020

This paper presents a risk assessment methodology for standard flight procedures using recorded automatic dependent surveillance-broadcast (ADS-B) data. Utilizing the proposed methodology, the results of risk analyses in RKSI (incheon international airport) and RKSS (gimpo international airport) using trajectories that are regenerated based on 100 days of ADS-B data are presented. For the risk metric, detect and avoid well clear (DWC) is used. With this index, each procedure was evaluated for the sections with highest level of risk. Among the standard instrument departure (SID) of RKSI, the section between SI712 and RANOS of RNAV BOPTA 1L showed the highest level of risk. For the standard terminal arrival route (STAR) of RKSI, section between SI947 and DANAN of RNAV GUKDO 1N wasthe one with the highest level of risk. For RKSS, the segment between SS726 and SS727 of RNAV BULTI 1X and the segment between KAKSO and KALMA of RNAV OLMEN 1D showed the highest level of risk among the SIDs and STARs, respectivly.

• Journal of Aerospace System Engineering
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• v.13 no.3
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• pp.70-77
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• 2019

This study presents the numerical investigation of the trajectory of rocket launched from a helicopter. The nonlinear mathematical model of armed configuration of UH-60 helicopter was developed while Hydra 70 unguided rocket was modeled to simulate the rocket behavior. The effects of various inflow models on the launched rocket trajectory are obtained. Similarly, rocket launch simulation was performed to determine the unsafe flight maneuver condition where the rocket trajectory is critically close to the helicopter main rotor tip path plane.

• Journal of Aerospace System Engineering
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• v.15 no.5
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• pp.50-59
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• 2021

The need for risk based safety management has been highlighted in accordance with the growth of aviation industry and public interest in aviation safety. Maintenance, Repair and Overhaul (MRO) in aviation industry is defined to guarantee the safety and reliability. Therefore, state's Civil Airworthiness Authority (CAA) has established safety oversight system dedicated for the development of a healthy MRO industry. The study proposed a risk based oversight system considering Korean environment. Based on literature review including analysis of International Civil Aviation Organization guidance and advance system, we identified two organization risks. Organization complexity can be evaluated in accordance with how large the organization is and how complicated the service they provide are. Organization profile is the organization's characteristic related with safety. This study contributes to improving the process of identifying risk of organization and focusing surveillance capabilities on risk areas for efficient management of CAA's resources.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.551-554
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• 2012

KARI is now developing KSLV-II which can insert 1.5ton satellite into the orbit, and system design review is close at hand. As a part of mission assurance for space launch vehicle, reliability and safety management is being performed and to assure the safety, KARI has been doing actions on the basis of the safety assurance plan and system safety program plan. In this study, preliminary hazard analysis is reviewed and the result for the propulsion system will be illustrated. The result will be used as a reference for the safety and risk management.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.3
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• pp.280-287
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• 2010

The first Korean satellite launch vehicle, KSLV-I(Korea Space Launch Vehicle-I), was launched for its first flight test on Aug. 25, 2009 from Naro Space Center located in south Jolla province. Because launch vehicles usually fly long range with large amount of propellants aboard, preparation of countermeasures against potential malfunctions during flight is essential in launch operation. In this paper, the flight safety operation, prepared to guarantee flight safety during launch operation of KSLV-I, is presented. Prior to flight test, flight safety analysis is performed to estimate associated risk levels quantitatively, and during flight, flight safety systems are operated to cope with any risky situations. Real-time flight monitoring including computation of instantaneous impact point using tracking data is executed normally and the flight test is completed without activation of flight termination system.

• Journal of Advanced Navigation Technology
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• v.23 no.1
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• pp.1-7
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• 2019

Thisstudy presentsthe development of a fast-time airport surface simulator. The simulator usesthe output from a first-come first-served (FCFS) scheduler and has adopted one-dimensional dynamic model to simulate the movement of the aircraft on the surface. Higher collision risks situations in the airport surface traffic are analyzed to classify those situations into six cases. A conflict detection and resolution algorithm is implemented to maintain separation distance and to prevent deadlock. The simulator was tested with a scenario at the Incheon International Airport that contains 72 aircraft. Without the conflict detection and resolution, various conflict situations are identified. When the conflict detection and resolution algorithm is managing the traffic, it is confirmed that the conflicts are removed at the price of additional delays. In the conflict resolution algorithm, three prioritization strategies are implemented, and delayed aircraft count and average additional delays are compared. Prioritization based on remaining time or distance showed smaller total additional delay compared to choosing minimum delay priority for each situation.

• Current Industrial and Technological Trends in Aerospace
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• v.9 no.1
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• pp.102-109
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• 2011

NEOs are comets and asteroids that have been nudged by the gravitational attraction of nearby planets into orbits that allow them to enter the Earth's neighborhood. When the NEOs with certain size impact in the Earth's surface, it could cause a serious disaster. However, the NEOs that are potentially the most hazardous because they can closely approach the Earth are also the objects that could bemost easily exploited for their raw materials. This paper presents the characteristics of NEOs and the technology trend of advanced countries on spacecraft missions to comets and asteroids.