• Aerospace Engineering and Technology
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• v.12 no.1
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• pp.128-136
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• 2013

Recently, the localization recognition system research has been studied using various sensors according to increased interest in autonomous navigation flight. In case of indoor environment which cannot support GPS information, we have to look for another way to recognize current position. The Image-based localization recognition system has been interested although there are lots of way to know current pose. In this paper, we explain the localization recognition system based on mark and implementation of autonomous navigation flight. In order to apply to real environment which cannot support marks, localization based on real-time 3D map building is discussed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.647-650
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• 2017

As the necessity of development of supersonic vehicle increases, securing an aerodynamic data from low to high altitude is requested for flying vehicles crusing in various high-tech environment. Therefore our research team built equipment by improving heating device of Model Aerodynamic Facility(MAF) of Konkuk University to simualte a real gas environment. Guided weapon system and temperature and velocity distribution according to the flow that is produced from the pier of supersonic vehicle is planned to be researched by using this equipment.

• Bulletin of the Korean Space Science Society
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• 2011.04a
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• pp.32.1-32.1
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• 2011

이 논문에서는 저궤도 지구관측위성 비행모델의 정현파 가진시험 결과에 대하여 분석하였다. 정현파 가진시험은 발사환경시험중의 하나로서, 저주파 대역의 정현파 진동 환경하에서 인공위성의 안정성을 검증하는데 그 목적이 있다. 정현파 가진시험의 입력선도는 발사체로부터 선정되어진다. 발사체로부터 선정된 입력선도는 극한의 경우를 고려한 선도이므로 실제 정현파 가진시험시에는 입력선도에 적절한 노칭을 적용하여야 한다. 노칭은 주구조물의 대한 1차 노칭과 부가 구조물에 대한 2차 노칭으로 구분이 되어 적용되었다. 정현파 가진시험의 전후에는 저수준 정현파가진시험을 수행하였으며, 주파수 응답함수를 비교함으로서 구조적으로 문제가 없는지를 확인하였다. 시험 후, 육안검사를 통하여 구조 부재가 이상이 없는지를 최종 확인하였으며, 인공위성비행모델이 정현파 가진 환경하에서 충분히 안전함을 확인하였다.

• Journal of the Korea Society for Simulation
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• v.27 no.4
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• pp.1-8
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• 2018

The most common way to control a target point using artificial intelligence is through reinforcement learning. However, it had to process complicated calculations that were difficult to implement in order to process reinforcement learning. In this paper, the enhanced Proximal Policy Optimization (PPO) algorithm was used to simulate finding the planned flight trajectory to reach the target point in the virtual environment. In this paper, we simulated how this problem was used to find the planned flight trajectory to reach the target point in the virtual environment using the enhanced Proximal Policy Optimization(PPO) algorithm. In addition, variables such as changes in trajectory, effects of rewards, and external winds are added to determine the zero conditions of external environmental factors on flight trajectory learning, and the effects on trajectory learning performance and learning speed are compared. From this result, the simulation results have shown that the agent can find the optimal trajectory in spite of changes in the various external environments, which will be applicable to the actual vehicle.

• Journal of Internet Computing and Services
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• v.15 no.1
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• pp.1-17
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• 2014

Flight software operated on the on-board computers in the satellite has requirements such as real-time, high reliability. These requirements make dependency between the flight software and operating environments. Further, whenever a new system is built, such problem drives that all flight software are redeveloped. Thus, the dependency problem between them should be solved. And the problem can be resolved by improving the portability of the flight software. In order to improve the portability it is required to minimize the porting cost. In this paper, we classify the portability with the portability achieving methods. Using the classified portability, we propose a platform architecture that is based on the IMA concept and provides various portability capabilities. The proposed architecture enables us to solve the problem about the development of the flight software.

• Journal of Aerospace System Engineering
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• v.14 no.spc
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• pp.39-48
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• 2020

This paper deals with the process of estimating the environmental noise generated from the actual flying aircraft using the noise measurement results obtained through the wind tunnel test and verifying it through flight tests. In order to evaluate the environmental noise of an aircraft, noise tests and evaluations are generally conducted according to the procedures prescribed by the International Civil Aviation Organization (ICAO). In this paper, we introduced environmental noise evaluation method that can be applied to composite both fixed-wing aircraft and multi-copter, and introduced the evaluation method by experiment. This paper introduces the process of simulating the noise test results measured in the wind tunnel test using real flight test results. In addition, in consideration of flight operating conditions and noise measurement methods proposed by the ICAO, the effective perceived noise level (EPNL) was predicted by performing both the wind tunnel test and the aircraft flight test.

• Journal of Digital Convergence
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• v.17 no.4
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• pp.365-379
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• 2019

The purpose of this study is to investigate what factors affect cyber-delinquency after examining the previous research focusing on the general strain theory and the delinquency opportunity theory in the existing studies. And as adolescents move from middle school to high school, this study is intended to analyze what factors affect cyber-delinquency from a longitudinal perspective using KCYPS(Korea Child and Youth Panel Survey) elementary 4th grade fourth and seventh data. The adolescence cyber-delinquency probability of occurrence were analyzed through the panel logit fixed-effect model using STATA. And then the cyber-delinquency frequency of adolescents were analyzed through the panel tobit random-effect model. As a result of analyzing the factors affecting cyber-delinquency frequency, Adult media commitment, computer use time, and cell phone dependency increased cyber-delinquency frequency. On the other hand, among the parenting attitudes, the attitude of supervising attentively and adolescents' age-increasing decreased cyber-delinquency frequency.

• 한국항공운항학회:학술대회논문집
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• 2016.05a
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• pp.5-8
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• 2016

본 연구에서는 다양한 급의 항공기를 단일 플랫폼에서 모의할 수 있는 시뮬레이터를 개발하기 위해 표준 비행역학 모의모델의 구조 및 인터페이스를 설계하였다. 비행역학 모의모델은 다양한 급의 항공기를 모의하기 위해 공통적으로 적용할 수 있는 비행동역학 모델과 환경모델은 항공기 기종에 관계없이 동일하게 설계하였고, 엔진, 구동기, 비행제어, 랜딩기어 모델과 같이 항공기 기종에 따라 차이가 있는 모델은 사용자가 선택하여 사용할 수 있도록 설계하였다. 또한 복잡한 구조의 소프트웨어를 사용자가 쉽게 접근하여 수정/모의할 수 있도록 비행역학 모의모델의 입력파일을 텍스트 기반인 XML 형식으로 설계하였다.

• KIPS Transactions on Software and Data Engineering
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• v.2 no.5
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• pp.353-358
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• 2013

In this paper, we present an implementation of indoor flight to navigate to the designated places capable of hands-off autonomous operation within indoor environments. Our flight requires computer vision technique and smartphone device to allow it to be flown indoors without high-performance sensors which are too expensive to commercialization. The experimental result show that proposed implementation is fairly meaningful in a general building.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.9
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• pp.867-873
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• 2008

Model based virtual Flight Control System construction is essential for Fly-by-Wire Flight Control System verification & validation(V&V) of concurrent engineering base. We researched the concept of dual-architecture system for virtual system construction, and analyzed Flight Control System that is applied to high altitude long endurance(HAE) UAS. Finally, we constructed the model based virtual Flight Control System with system analysis and achieved system verification about flight critical failure modes. Analysis target is RQ-4A.