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Hypervelocity Impact Simulations Considering Space Objects With Various Shapes and Impact Angles 考虑不同形状和角度空间物体的超高速碰撞仿真
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.829
Hyun-Cheol Shin, Jae-Sang Park
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引用次数: 0
Parallel Computation on the Three-dimensional Electromagnetic Field by the Graph Partitioning and Multi-frontal Method 三维电磁场的图划分与多面并行计算
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.889
Seung-Hoon Kang, Dong-Hyeon Song, Jaewon Choi, Sang-Joon Shin
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引用次数: 0
Review of the Sintering Technologies Using In-situ Resources for Lunar Construction and Future Works 月球建设及未来工程中就地资源烧结技术综述
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.839
G. Ryu, Youngjae Kim, H. Shin
Over the last decade, the competition for space development has accelerated. The world's largest space agencies are aiming toward long-term lunar exploration and manned missions. For sustainable and safe lunar exploration, construction of infrastructures that include various habitats is
在过去十年中,空间开发的竞争加速了。世界上最大的航天机构正致力于长期月球探测和载人任务。为了实现可持续和安全的月球探索,包括各种栖息地在内的基础设施建设是至关重要的
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引用次数: 0
Analysis of Low Altitude Wind Profile Data from Wind Lidar for Drone Aviation Safety 基于风激光雷达低空风廓线数据的无人机飞行安全分析
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.899
Jewon Kim, J. Ryu, Seon-Jun Na, Seong-Cheol Seong
According to the Unmanned aircraft system Traffic Management (UTM), drones are permitted to fly up to 150m above ground, which is located in the atmospheric boundary layer where there is considerable wind fluctuation due to turbulence. Although it is difficult to predict when turbulence will occur drone aviation safety could be enhanced by having a better understanding of the characteristics of vertical profile of wind in the flight area. We used wind lidar (WIndMast 350M) to observe vertical profiles of wind at the test site for aviation meteorological observation equipment located near Incheon International Airport in July and September, 2022. In this study, we utilized the observed wind profile data to propose a technique for obtaining information that could help improve the drone aviation safety. The Fourier transform analysis is used to evaluate the temporal characteristics of the horizontal wind speed at various vertical levels up to 350m. We also examined the relative contribution of the variance of wind having scales of less than an hour, a crucial scale for drone flight, to the variance of wind having all scales at each vertical altitude for days with and without precipitation
根据无人机系统交通管理(UTM),无人机被允许在距离地面150米的高空飞行,这是位于大气边界层中,由于湍流而有相当大的风波动。虽然很难预测湍流何时会发生,但通过更好地了解飞行区域的垂直风廓线特征,可以提高无人机的飞行安全性。我们于2022年7月和9月在仁川国际机场附近的航空气象观测设备试验场,利用风激光雷达(WIndMast 350M)观测了风的垂直剖面图。在本研究中,我们利用观测到的风廓线数据,提出了一种获取信息的技术,可以帮助提高无人机的飞行安全性。利用傅里叶变换分析评价了350米以下不同垂直高度水平风速的时间特征。我们还研究了在有和没有降水的日子里,小于一小时尺度的风的方差对每个垂直高度上所有尺度的风的方差的相对贡献,这是无人机飞行的关键尺度
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引用次数: 0
Preliminary Mission Design of Transfer Orbit of a Lunar Lander Launched by a Korean Space Launch Vehicle 韩国空间运载火箭发射的月球着陆器转移轨道初步任务设计
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.867
Eun-Jung Song, Sang-il Lee, Jiyoung Choi, Byung-Chan Sun, Woong-Rae Roh
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引用次数: 0
Battery Sensitivity Analysis on Initial Sizing of eVTOL Aircraft eVTOL飞机初始尺寸电池灵敏度分析
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.819
Minjung Park, Jou-Young Choi, Se-Hwan Park
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引用次数: 0
Modeling of Fixed Wing UAV and Flight control Computer Based Autopilot System Development for Integrated Simulation HILS Environment 集成仿真HILS环境下固定翼无人机建模与飞控计算机自动驾驶系统开发
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-12-31 DOI: 10.5139/jksas.2022.50.12.857
Lamsu Kim, Dongwook Lee, Hohyeong Lee, Suwoon Hong, Hyochoong Bang
{"title":"Modeling of Fixed Wing UAV and Flight control Computer Based Autopilot System Development for Integrated Simulation HILS Environment","authors":"Lamsu Kim, Dongwook Lee, Hohyeong Lee, Suwoon Hong, Hyochoong Bang","doi":"10.5139/jksas.2022.50.12.857","DOIUrl":"https://doi.org/10.5139/jksas.2022.50.12.857","url":null,"abstract":"","PeriodicalId":42856,"journal":{"name":"Journal of the Korean Society for Aeronautical and Space Sciences","volume":"10 1","pages":""},"PeriodicalIF":0.2,"publicationDate":"2022-12-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"88611585","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Multiple Drones Collision Avoidance in Path Segment Using Speed Profile Optimization 基于速度轮廓优化的多无人机路径段避碰
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-11-30 DOI: 10.5139/jksas.2022.50.11.763
Tae-Hyoung Kim, T. Kang, Jin-Gyu Lee, Jong-Han Kim, C. Ryoo
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引用次数: 0
Helicopter Active Airframe Vibration Control Simulations Using an Exhaustive Test Method 基于穷举试验方法的直升机主动机身振动控制仿真
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-11-30 DOI: 10.5139/jksas.2022.50.11.791
Byeong-Hyeon Park, Ye-Lin Lee, Jae-Sang Park
{"title":"Helicopter Active Airframe Vibration Control Simulations Using an Exhaustive Test Method","authors":"Byeong-Hyeon Park, Ye-Lin Lee, Jae-Sang Park","doi":"10.5139/jksas.2022.50.11.791","DOIUrl":"https://doi.org/10.5139/jksas.2022.50.11.791","url":null,"abstract":"","PeriodicalId":42856,"journal":{"name":"Journal of the Korean Society for Aeronautical and Space Sciences","volume":"90 1","pages":""},"PeriodicalIF":0.2,"publicationDate":"2022-11-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"83550544","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A Study of the Influence of the Injection Location of Supersonic Sweeping Jet for the Control of Shock-Induced Separation 超音速掠流射流喷射位置对冲击分离控制的影响研究
IF 0.2 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-11-30 DOI: 10.5139/jksas.2022.50.11.747
S. Park, Yeol Lee
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引用次数: 0
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Journal of the Korean Society for Aeronautical and Space Sciences
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