This study investigates the effects of digital interface structure on the operational performance of unmanned and manned–unmanned integrated mechanical systems from a human factors perspective. Using case-based comparative analysis, changes in response time, operation error rate, and situational awareness accuracy before and after interface redesign were examined. The results indicate that improvements in interface integration, procedural simplification, and consistency significantly enhance operational performance without modifying mechanical hardware or control algorithms. The study highlights the importance of incorporating human factors engineering into the early design and evaluation stages of complex mechanical systems.

Modern warfare demands a high level of coordination and interoperability among multiple combat vehicles and crew members operating in dynamic and complex environments. Traditional training methods are often limited in scalability, flexibility, and cost-efficiency, making it challenging to effectively prepare forces for future battlefield scenarios. To address these limitations, this study presents the development of a Multiple Combat Vehicle Integrated Training Device, a next-generation simulation-based training system. The MCITD integrates advanced technologies such as Extended Reality, Digital Twin modeling, and Artificial Intelligence to deliver immersive, interactive, and highly realistic training experiences. The system allows for simultaneous training of multiple crew members in a networked environment that replicates real-world combat conditions, including terrain, weather, and adversary behavior. Key system components, including the simulation module, network communication framework, battlefield environment generator, and performance analysis engine, are discussed in detail. Potential application scenarios such as large-scale land operations, urban warfare, and multinational joint training exercises are also explored. The MCITD aims to enhance combat readiness, mission success, and training efficiency by providing a cost-effective, scalable, and adaptable solution for future-oriented military training programs.

This study explores the critical interrelationship between component standardization and airworthiness certification in the context of military aircraft systems. As the complexity and technological integration of modern defense platforms increase, the alignment between standardized component frameworks and evolving airworthiness requirements becomes essential to ensure operational reliability, safety, and maintainability. The current defense acquisition and certification systems often operate in a decoupled manner, leading to duplicated testing, certification delays, and cost overruns. Through comparative analysis of national and international certification protocols (MIL-HDBK-516, NATO STANAG, EASA SIB), this paper identifies structural inefficiencies in managing non-standardized or partially certified components. Based on these findings, the study proposes a function-based integrated management system that enables data synchronization across standard parts databases, quality records, and certification requirements. The proposed framework consists of four core modules: (1) standard part information management, (2) quality assurance and test linkage, (3) certification support engine, and (4) lifecycle risk monitoring. The study also anticipates quantifiable improvements such as reduced certification time and improved audit traceability. The results provide practical and policy implications for enhancing the interoperability, reliability, and export competitiveness of domestic defense platforms.

As modern weapon systems become increasingly complex, the need for integrated management of component standardization and airworthiness certification has grown significantly. This study proposes a system-based approach to establish an integrated management framework that addresses inefficiencies, certification delays, and supply chain risks inherent in current military aircraft development processes. The research reviews the functional scope of component standardization and compares airworthiness certification systems across domestic and international defense sectors. It identifies limitations caused by the fragmented management of parts and certification processes, and proposes a digital platform that interconnects parts databases, configuration control, quality assurance, and certification modules. The framework incorporates AI and digital twin technologies to monitor and manage reliability across the entire life cycle of a weapon system. This study lays the foundation for enhancing the operational efficiency of national defense technologies, and contributes to strengthening the autonomy and global competitiveness of the Korean defense industry.

This study examines the effects of additive manufacturing (AM) orientations and support structures on the compressive strength of lattice structures. Test specimens were fabricated using a selective laser melting (SLM) process with AlSi10Mg material under three conditions: horizontally aligned (0°), tilted at 45°, and supported. Compression tests were conducted using a universal testing machine (UTM) and Digital Image Correlation (DIC) to evaluate mechanical behavior. The results showed that the supported horizontal specimens exhibited the highest compressive strength, while the 45° tilted specimens had the lowest due to interlayer separation and localized failures. The findings highlight the significance of build orientation and support design in optimizing AM lattice structures. Future research should explore various lattice configurations, material selections, and post-processing effects to further enhance structural performance.

본 논문은 선박·항만안전과 운항(영)의 효율성 확보를 위해 도입된 강제도선의 법적 문제점을 검토하고, 관공선 운항 사례를 중심으로 그 적용상의 불합리성과 형평성 문제를 분석하였다. 해군 및 해양경찰 함정의 경우, 별도의 군 도선사 제도와 자력도선을 통해 묵시적으로 강제도선 적용을 배제하고 있으나, 이는 법령상의 명확한 근거 없이 행정해석에 의존하는 문제를 야기하여 법률유보원칙과 예측가능성에 저촉되는 것으로 보인다. 또한, 관공선 중 실습선만 유일하게 동일한 공익 목적에도 불구하고 차별적 규제가 적용되어 자의 금지원칙 및 평등 원칙에 저촉됨을 확인하였다. 이에, 본 연구는 강제도선 적용 대상 및 예외 규정을 명확히 하고, 운항목적·안전성 평가· 승무원의 숙련도 등을 종합적으로 고려한 세부기준 마련의 필요성을 제시하며, 실습선의 경우 도선구 내 항로 사용을 한정한 자력도선 허용 방안과 이외 관공선은 강제도선 면제에 관한 법적 근거를 마련하는 것을 입법적 개선안으로 제안하였다. 추가로 실습선의 경우 향 후 사고 없이 항만 내에서 선박운항을 수행한다면 다른 관공선과 함께 전면적인 강제도선 면제방안을 제시하는 것도 법리적으로 혹은 비 교법적으로도 무리는 없어 보임으로 추가적인 개정안을 제안하였다.

2019년 발생한 코로나 팬데믹은 백신의 지역별 불평등 분배를 야기하며 백신의 수급은 사회･정치적 문제로 확장되어 왔다. 의료 자원에 대한 공급과 수요를 예측하고 조정하는 것은 향후 발생할 수 있는 팬데믹 위기 해결의 실마리가 된다. 본 연구는 백신이라는 한정된 의료 자원의 공간적 형평성을 달성하는 것을 목적으로, 머신러닝을 통해 미래 서울시 인구 및 공간적 백신 접근성을 예측하였다. 공간분석 분야에서 공간접근성을 측정하는 데에 통용적으로 활용되는 2SFCA(Two-Step Floating Catchment Area Method) 방법론으로 백신의 공급처인 병원의 접근성을 파악하였다. 2017년 부터 2023년까지의 백신 접근성 및 백신 취약지를 도출한 뒤, 발생 핫스팟(Emerging Hot Spot) 탐색으로 과거부터 미래까지의 분포 변화를 분석하였다. 대한민국 의료 거점지인 서울시 백신 접근성의 측정 결과, 향후 백신 접근성은 전역적으로 감소할 것으로 보이며 특히 북부지역 비롯한 외곽지역이 접근성 취약지역으로 판단되었다. 본 연구는 서울의 시공간적인 백신 공급을 예측 및 분석하여 향후 발생할 수 있을 팬데믹 상황에 대비한 백신 취약지를 보완할 수 있는 지표를 완성하였다. 연구 결과는 백신 취약지역을 효과적으로 탐색할 수 있을 뿐만 아니라 미래 효과적인 백신 분배 정책에 기초자료로 활용할 수 있을 것이라 기대한다.

This paper delves into the standard system for selecting aviation tools. Generally, standards are seen as foundational and fundamental. However, in actual practice, there are often instances where a thorough differentiation of the standard unit system isn't properly executed, resulting in product defects in certain companies. Therefore, through the insights gathered in this study, we aim to reaffirm the basic principles and move forward with the objective of manufacturing products of impeccable quality in accordance with future quality improvement policies. Ultimately, we aspire for K-Defense to emerge as a prominent leader in the global market.

This paper studied a new shape unit model based on Gibson and Ashby's theory. As a result of theoretical research, the relative density equation is correlated with relative elasticity, and through this study, the theoretical relationship between the relative elasticity equation was defined. The relative elasticity equation was defined based on the model for which the analysis was performed. According to the analysis results, the diameter of the model was set to 3 mm, and the maximum stress values were confirmed by reflecting the same boundary conditions. The maximum stress for each model is 5668.9MPa for Type 1, 5136.7MPa for Type 2, 5642MPa for Type 3, and 6032.9MPa for Type 4 when the truss diameter is 3mm. The relative elasticity equation was defined based on this condition. In the future, compression analysis will have to be performed in the same way, reflecting the diameter of the truss at 5 mm and 7 mm, to find and define the coefficients of the relative elasticity equation, and verification through experiments will have to be carried out based on the theoretical equation. In addition, in order to be applied in each field, proof through prototype production and installation must be carried out.

본 연구는 자일로올리고당의 과학적이고 체계적인 표준 화된 시험법을 마련하여 다양한 제형의 제품에 적용하고 자 하였다. 최적화된 시험법을 마련하기 위해 초음파 처 리 시간, 산 가수분해 시간 및 농도를 검토하여 전처리 방 법을 비교 평가하였으며, HPLC-UVD를 이용하여 시료 중 의 자일로올리고당을 분석하였다. 분석 시 1-phenyl-3- methyl-5-pyrazoline (PMP)으로 유도체화하고, photo diode array (PDA)가 장착된 high performance liquid chromatography (HPLC) (Nanospace SI-2)를 사용하였으며, 칼럼은 Cadenza C18 (4.6 × 250 mm, 3 μm)이었으며, 이동상은 pH를 6.0으 로 맞춘 20 mM 인산완충용액과 아세토니트릴을 78:22 비 율로 혼합하여 사용하였고, 0.5 mL/min 유속으로 254 nm 로 하여 분석하였다. 건강기능식품 등 시험법 마련 표준 절차에 관한 가이드라인에 따라 밸리데이션을 수행하고, 표준화된 시험법을 이용하여 유통 중인 건강기능식품 대 상 품목에 대해 시험법 적용 여부를 확인하였다. 표준화 된 시험법은 자일로올리고당을 함유한 건강기능식품 품질 관리에 대한 신뢰성을 더 높일 것으로 본다.

본 연구는 그린커피빈추출물이 「건강기능식품의 기준 및 규격」에 추가로 등재될 경우를 대비하여 표준화된 클 로로겐산 시험법을 설정하고, 카페인이 동시 분석되도록 최적화하는 연구를 진행하였다. 최적화된 시험법을 마련 하기 위해 기기분석 및 전처리 조건을 비교·분석하여 클 로로겐산과 카페인을 30% 메탄올 추출하여 인산용액과 인산 함유 아세토니트릴으로 액체크로마토그래프를 통해 330 nm, 280 nm에서 분석하도록 시험법을 설정하였다. 시 험법 밸리데이션 결과, 직선성 정량범위 내에서 상관계수 (R2) 0.999 이상의 유의수준을 보였고, 클로로겐산과 카페 인 검출한계는 0.5와 0.2 μg/mL, 정량한계는 1.4와 0.4 μg/ mL로 나타났다. 정밀도와 정확도 결과는 AOAC 밸리데 이션 가이드라인를 통해 적합함을 확인하였고, 클로로겐 산 및 카페인 동시분석법을 최종적으로 마련하였다. 또한, 시제품과 유통제품을 통해 제형별 적용성 검토하여 클 로로겐산과 카페인을 동시에 정량 가능한 시험법임을 재확인하였다. 최적화된 시험법은 클로로겐산을 함유한 건강기능식품 품질관리에 대한 신뢰성을 더 높일 것으 로 본다.

This study divided the coast of Gyeongsangnam-do into three specialized base areas to revitalize tourism on the southern coast and suggested using AAM for movement within base areas. It analyzes the feasibility of advanced transportation means to revitalize coast tourism. It presents a new perspective and the environmental change in the tourism field. The results of this study are expected to have great implications in that it’s applicable to all marine tourism on the southern coast, including Jeollanam-do and Busan, beyond Gyeongsangnam-do.

This study compares and analyzes the drogue shape applied to aerial refueling with the U.S. Navy drog shape through basic analysis of the model based on the flying fish shape, a marine creature. Flying fish is a creature that is advantageous for non-powered downhill, and this shape is applied to the probe feeding method to minimize the burden on the pilot and the need for refueling technology, which are disadvantages of the probe method. To this end, the results through analysis of basic studies were confirmed, and the superiority and insufficiency of the flying fish shape model and the US Navy drogue model were compared. Therefore, as confirmed through analysis, the flying fish model had a 14.1% lower maximum air pressure and a 9.1% faster maximum speed. Based on this, it is hoped that the advantages and disadvantages of flying fish shape models will be confirmed through actual flight tests in the future.

The purpose of this paper is to propose part management and standardization to reduce cost and increase compatibility of parts through standardization and standardization of parts to be applied to urban air mobility(UAM) systems, Personnel Air Vehicle(PAV), Vertical Take-Off and Landing (VTOL), and so on. In other words, parts used in the urban air transportation system must be verified from the initial design stage in accordance with the aviation standard, and a systematic management system for various parts must be established to secure stability and improve quality. Therefore, as a system similar to the aviation component management system, it should be thoroughly managed for urban aviation components.

This paper intends to consider the contents of the insufficient certification system of PAV and to propose the certification regulations. In other words, PAV is a combination of people and drones that should reflect commercial specifications among aviation certification specifications and civil aircraft regulations. However, the domestic PAV certification system is still lacking in clear detailed regulations, and the detailed certification system of PAV should be established as soon as possible. It is hoped that PAV certification system will be established first and applied in earnest in the future, and that the domestic PAV industry will be activated.