• 한국국방경영분석학회지
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• 제2권1호
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• pp.177-184
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• 1976

As the organizational size of a military service or business increases and its management becomes complex, the success in its management depends less on static type of management but more on careful, dynamic type of management. In this thesis, an operations research technique is applied to the problems of determining optimal air traffic control rule and of optimal capacity of air base for a military air base. An airport runway is regarded as the service facility in a queueing mechanism, used by landing, low approach, and departing aircraft. The usual order of service gives priority different classes of aircraft such as landings, departures, and low approaches; here service disciplines are considered assigning priorities to different classes of aricraft grouped according to required runway time. Several such priority rules are compared by means of a steady-state queueing model with non-preemptive priorities. From the survey conducted for the thesis development, it was found that the flight pattern such as departure, law approach, and landing within a control zone, follows a Poisson distribution and the service time follows an Erlang distribution. In the problem of choosing the optimal air traffic control rule, the control rule of giving service priority to the aircraft with a minimum average waiting cost, regardless of flight patterns, was found to be the optimal one. Through a simulation with data collected at K-O O Air Base, the optimal take-off interval and the optimal capacity of aircraft to be employed were determined.

• Journal of Platform Technology
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• 제9권3호
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• pp.24-35
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• 2021

고속의 군용 항공기는 인명피해 최소화를 위해 생존 장비들과 경고 시스템으로 적의 위협 또는 내부 구성품 불량을 조종사가 파악하고 해결할 수 있어야 한다. 경고 전달은 디스플레이에 심볼 전시를 통한 시각적 방법과 통신 장비의 소리를 통한 청각적 방법으로 구분되는데, 청각적 방법이 반응 시간이 짧고 단순한 메시지 청취를 통해 조종사 혼란을 유발하지 않는다는 점에서 우월하다. 이에 본 논문은 군용 항공기용 음성/톤 경고 시스템의 효과적인 설계방법을 생명주기 관점에서 제시하고 평가하였다. 안전에 민감한 군용 항공기이므로 각 경고에 우선순위와 Inhibitible, Interruptible, Deactivatable의 세 가지 속성들을 적용하여 중대성과 긴급성을 반영했다. 그 결과 음성경고 재생까지 40ms가 소요되었으며, V모델 기반 개발 및 테스트를 통해 요구도를 모두 충족했고 제품 신뢰성이 향상됨을 확인하였다.

• 한국군사과학기술학회지
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• 제25권6호
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• pp.572-579
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• 2022

The analysis of foreign aircraft appearing suddenly in air defense identification zones requires a lot of cost and time. This study aims to develop a pre-trained model that can identify neighboring military aircraft based on aircraft photographs available on the web and present a model that can determine which aircraft corresponds to based on aerial photographs taken by allies. The advantages of this model are to reduce the cost and time required for model classification by proposing a pre-trained model and to improve the performance of the classifier by data augmentation of edge-detected images, cropping, flipping and so on.

• 한국군사과학기술학회지
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• 제15권6호
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• pp.738-745
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• 2012

Aircraft battle damage repair(ABDR) is emergency repair method for the damaged aircraft in battle field. The main purpose of the ABDR is to increase the readiness of fighter aircraft during wartime. While many studies have been conducted to develop ABDR method, few efforts have focused on evaluation of damage and determination of the size of hole caused by enemy's anti-aircraft artillery attack. The aim of this study is essentially to quantify damage of aircraft wing attacked by anti-aircraft artillery. The computer simulations was performed to accomplish this goal. A number of simulations have been carried out to compare size of damages under various attack conditions. In conclusion, it was revealed that the size of damage varied depending on the type and direction of cannonball. Furthermore, in this paper, the proper path sizes are suggested for different damage conditions.

• 품질경영학회지
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• 제47권3호
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• pp.467-478
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• 2019

Purpose: The purpose of this paper is to improve quality for water infiltration to FCISA during military aircraft operation. Methods: A series of troubleshooting studies were conducted to identify the root cause of the water infiltration and reproduce the defects through various simulation tests. And design improvement measures were derived, and countermeasures were taken to prevent recurrence of moisture inflow defects. Conclusion: FCISA operates a very important role in the operation of military aircraft, and defects due to water infiltration are very fatal to flight safety. In this study, the root cause was identified and the design improvement to prevent recurrence was carried out through the failure investigation performed in this study, and the FCISA was improved so that the flight safety was not affected. The results of this study will be valuable back data that can be reflected in the design process through Lessons-Learned in the design phase of the aircraft that will be developed in the future.

• 한국군사과학기술학회지
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• 제12권2호
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• pp.248-257
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• 2009

The aim of this paper is to propose fighter aircraft's mission severity model which can be used as one of key factors for designing a structure and determining design life of KF-X. The mission severity is a quantitative data of flight loads and expressed by Nz(Vertical Load Factor) exceedances or occurrences. The severities of the flight loads depended on the circumstances of the countries which operate fighter aircraft. In this paper we have studied on Nz occurrences/exceedances of ROKAF fighter aircraft to generate mission severity model for the KF-X. The analyses of flight data were accomplished by using the Matlab.

• 품질경영학회지
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• 제41권3호
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• pp.423-432
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• 2013

Purpose: A Study on the application of quality management system specification to production validation and audit in military airworthiness certification. Methods: Aircraft quality management system specification for quality assurance and production validation and audit requirements were examined to verify. Also, the system for domestic and foreign production certification were investigated. Results: Production validation and audit criteria for military aircraft by applying methods suggested Aircraft Certifications Systems Evaluation Program(ACSEP). ACSEP evaluation of the items, some items were complementary and not applied. Conclusion: As a way to ensure the safety of aircraft, confirm the correction of Production validation & audit criteria and rulemaking is necessary and how to manage for Critical Safety Item(CSI) is a need to improve.

• 한국군사과학기술학회지
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• 제14권3호
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• pp.397-404
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• 2011

The aerodynamic characteristics of a separated captive body in flow field around aircraft are studied to observe aerodynamic stability for safe separation from aircraft. Since the captive body separated from aircraft is initially exposed to unsteady flow pattern, the change of aerodynamic forces and moments should be measured to analyze how the flow pattern affects on the captive body at the vicinity of aircraft. Aerodynamic forces and moments of the separated captive body are measured at selected positions along predictable dropping trajectories. The measuring trajectories, generated by the free drop test of the dropping model in the wind tunnel, are consisted of 9 possible lines by free dropped trajectories. Experimental results show that the aerodynamic forces and moments are significantly varied with the distance between the captive body and aircraft. In conclusion, the change of aerodynamic characteristics within flow field around aircraft should be considered to simulate trajectories of the separated captive body from aircraft.

• 한국군사과학기술학회지
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• 제24권6호
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• pp.638-644
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• 2021

Infrared guided weapons act as threats that greatly degrade the survivability of combat aircraft. Infrared weapons detect and track the target aircraft by sensing the infrared signature radiated from the aircraft fuselage. Therefore, in this study, we analyzed the infrared signature and susceptibility of supersonic aircraft according to omni-directional detection angle. Through the numerical analysis, we derived the surface temperature distribution of fuselage and omni-directional infrared signature. Then, we calculated the detection range according to detection angle in consideration of IR sensor's parameters. Using in-house code, the lethal range was calculated by considering the relative velocity between aircraft and IR missile. As a result, the elevational susceptibility is larger than the azimuthal susceptibility, and it means that the aircraft can be attacked in wider area at the elevational situation.

• 항공우주정책ㆍ법학회지
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• 제20권2호
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• pp.59-158
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• 2005

현재 공군이 보유하고 있는 군용항공기가 그 설계, 제조, 사용상의 주의사항 경고 누락 등과 같은 제조상의 결함으로 인하여 인적 혹은 물적 피해가 발생한 경우, 그 책임소재를 가려 항공기 제조회사 등 법적 책임이 있는 자에게 최종적 책임을 물어야하고 이러한 점은 당해 제조상의 결함에 추가적인 사고피해로 이어지지 않는 경우에도 마찬가지이다. 또한, 보다 중요한 것은 그와 같은 책임추궁을 하기에 앞서 군용항공기의 부품이나 완성품에 애초부터 하자가 발생하지 않도록 사전에 미리 조치하는 것이다. 그럼에도 불구하고, 현재 실무상 항공기의 제조상 결함에 대한 사전 방지대책이나, 사후의 결함발생에 대한 효과적이고 명확한 대응방안이 체계적으로 제시되지 않고있다. 즉, 현재 군수물자 조달에 관한 일반 실무지침이나 협상의 기준으로 제시되는 계약서 양식 및 관련 법령 및 제도는 군용항공기의 부품적 특성, 구매방식에 따른 협상의 난이 등을 실무적 관점에서 충분히 고려한 것이라고 보기 어렵고 또한, 군용항공기 결함에 대한 책임추궁 법리 연구도 실무장의 요구를 충족시키기에는 다소 부족한 실정이다. 따라서, 군용항공기의 제조상 결함과 관련된 국가의 법적 대응방안을 미리 확보해 놓는 것이 필요한데, 여기서의 법적 대응방안이라는 것은 크게 두 가지로 구분할 수 있다. 그 하나는 군용항공기의 결함이 발생하지 않도록 판매제조업체 선정시 구매방식상의 특성을 고려하여 보다 안정적인 부품 및 완성품을 공급받을 수 있는 법적제도적 방안을 마련하는 한편, 부품에 하자가 발생할 때를 대비하여 계약시에 그 책임을 물을 수 있는 충분한 법적 장치를 설치하는 것이다. 다른 하나는 그 와 같은 노력에도 불구하고 부득이하게 제품에 하자가 발생한 사후에 있어서 책임있는 자에게 법적 책임을 추궁하기 위한 법논리를 탄탄히 갖추는 일일 것이다. 따라서, 이 글을 통해 앞으로 군용항공기를 사전에 계약함에 있어서 구매방식에 따른 문제점을 짚어본 후 그에 대한 법적제도적 개선방안을 모색하고, 또한 항공기의 결함 및 그로 인한 사고 실제로 발생한 경우 이에 대한 분쟁을 처리함에 있어서의 법적 개선점을 찾아보고자 한다. 이렇게 함으로써 장기 방위전략사업 및 대규모 국책사업 성격을 띠는 군용항공기의 구매 시에 제품의 결함율을 감소시켜 국가방위전력을 향상시킴과 동시에 추후 하자발생으로 인한 막대한 국가 및 국민의 인적 물적 손실을 방지하는데 도움을 줄 수 있다고 본다. 이 글에서는 먼저 군용항공기의 구매방식에 따른 제품결함 발생과 관련한 문제점 및 결함발생 방지를 위한 사전 개선방안을 논하고, 결함이 실제 발생한 경우의 제조회사에 대한 정부 및 피해국민의 정당한 책임추궁 방법을 군용항공기의 특성을 고려하여 논의하도록 하겠다.