• Title/Summary/Keyword: 비행시뮬레이터

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Building Mixed Reality System for a VR Flight Simulator (비행 VR 시뮬레이터를 위한 혼합 현실 환경의 구축)

  • 이종환;한순흥
    • Journal of the Korea Society for Simulation
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    • v.13 no.2
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    • pp.45-52
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    • 2004
  • This paper presents a prototype visualization system of mixed reality for a VR flight simulator. The chroma key technique is used to build the mixed reality model for a VR flight simulator. The Daedeok science town can be visualized in real time according to the rider control. He can also see his own hand/foot operating the control stick/rudder as well as virtual environment projected to the blue-screen using a video-see-through HMD.

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고장 대응 훈련을 위한 시뮬레이터 고장 발생 메커니즘 소개

  • Lee, Hun-Hui;Gu, Cheol-Hoe;Ju, Gwang-Hyeok
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.194.1-194.1
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    • 2012
  • 우주비행체의 내부 장치 고장 혹은 외부 환경에 의한 고장이 발생할 경우를 대비하여 가상 모의 시뮬레이터를 이용한 고장 대응 훈련이 요구된다. 시뮬레이터 개발 초기에 이러한 고장 발생 메커니즘을 설계에 반영하지 않는 경우 교관이 작성한 고장 시나리오에 의한 유기적 고장 발생 및 고장 전파 기능을 납품 후 추가 요구하기는 용이하지 않다. 본 논문에서는 사용자가 시뮬레이터를 이용하여 의도하는 고장을 의미있는 시각(Epoch)에 주입하기 위한 고장 발생 메커니즘 구조를 설명한다. 또한 천리안위성 시뮬레이터 소프트웨어의 고장 발생 예제를 통해 고장 감지, 고장 복구, 관제원의 대응 방법 등을 설명한다.

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Development of Software for Fidelity Test of Flight Dynamic Model on Fixed Wing Aircraft (고정익 항공기의 비행역학 모델 충실도 테스트를 위한 소프트웨어 개발)

  • Baek, Seung-Jae;Kang, Mun-Hye;Choi, Seong-Hwan;Kim, Byoung Soo;Moon, Yong Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.8
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    • pp.631-640
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    • 2020
  • Currently, aircraft simulator has drawn a great attention because it has significant advantages of economic, temporal, and spatial costs compared with pilot training with real aircraft. Among the components of the aircraft simulator, flight dynamic model plays a key role in simulating the flight of an actual aircraft. Hence, it is important to verify the fidelity of flight dynamic model with an automated tool. In this paper, we develop a software to automatically verify the fidelity of the flight mechanics model for the efficient development of the aircraft simulator. After designing the software structure and GUI based on the requirements derived from the fidelity verification process, the software is implemented with C # language in Window-based environment. Experimental results on CTSW models show that the developed software is effective in terms of function, performance and user convenience.

A Study on the Development of Flight Simulator Training Device for the Prevention of Helicopter Flight Spatial Disorientation (헬리콥터 비행착각 예방을 위한 모의비행훈련장치 개발에 대한 연구)

  • Se-Hoon Yim
    • Journal of Advanced Navigation Technology
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    • v.27 no.2
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    • pp.155-161
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    • 2023
  • Vertigo refers to a state in which awareness related to the location, posture, movement, etc. of a helicopter is insufficient in space. It is easy to fall into flight illusion when flying in dense fog or night flight, and even if it has a wide field of view, it can be caused by visual causes such as cloud shapes, wind conditions, conditions of ground objects, and sensory causes such as changes in air posture or gravitational acceleration. The design and program of the motion system are studied that applied a six-axis motion system to a conventional commercial flight simulator program for pilot training, depending on the specificity of helicopter flight training that requires perception and sensitivity. Using the motion-based helicopter simulator produced in this study to train pilots, it is expected to have a positive effect in prevent of vertigo, where high performance could not be confirmed in the previously used visual-based simulation training device.

Development of FAA AC120-63 Level C Flight Simulation Model for KA-32T (FAA AC120-63 Level C급 KA-32T 비행 시뮬레이션 모델 개발)

  • Jeon, Dae-Keun;Jun, Hyang-Sig;Choi, Hyoung-Sik;Choi, Young-Kiu
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.4
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    • pp.406-412
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    • 2009
  • Flight simulation model for helicopter simulator is one of the most important models which affect flight performance and handling quality. It is typical to develop the model based on the raw data and models from the helicopter designers/manufacturers. The approaches in this study were to develop the basic model based on the available resources regarding helicopter operation/maintenance and to tune and validate it based on the flight test results. The basic model was developed with maintenance manuals, flight manuals, analyses, measurements, papers and so on considering that KA-32T data could not be obtained from the manufacturer. The flight test for KA-32T was performed and the reference data for the simulation validation tests were acquired. The flight simulation model was validated to have the fidelity compatible with level C of FAA AC120-63 after comparison and tuning with flight test results.

A Design of Handling Quality Assessment Environment Based on FLIGHTLAB Model Using Legacy Simulator (레거시 시뮬레이터를 활용한 FLIGHTLAB 모델 기반의 조종성 평가 환경 설계 연구)

  • Yang, Chang Deok;Lee, Seung Deok;Cho, Hwan Heui;Jung, Dong Woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.6
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    • pp.530-536
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    • 2016
  • The handling quality simulator including high fidelity flight mechanics model is indispensable component to design and verify the flight control system. Korea Aerospace Industries, LTD. (KAI) has been performing LCH (Light Civil Helicopter) core technology development program regarding automatic flight control system (AFCS) software development. And KAI has been developing flight mechanics model using FLIGHTLAB to design and evaluate the AFCS flight control law. This paper presents the handling quality assessment environment development results through the combining FLIGHTLAB with a legacy simulator. And this paper details the FLIGHTLAB model, application development process and FLIGHTLAB interface design. The developed handling quality assessment environment has been demonstrated with the ADS-33E hover and pirouette MTE (Mission Task Element) maneuver simulation.

Development of an FMCW Radar Altimeter Simulator Using Optical Delay Lines (광 지연선을 이용한 FMCW 전파고도계 시뮬레이터 개발)

  • Lee, Jae-Hwan
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.28 no.3
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    • pp.208-216
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    • 2017
  • This paper presents the design method of an FMCW(frequency-modulated continuous-wave) altitude simulator which generates propagation delay signals according to target distances to test the radar altimeter. To improve the conventional RF method for creating delay signals, the simulator is designed by the RF-optics-RF method using optical delay lines. In addition, it is designed to simulate the Doppler shift and jamming that may occur in actual flight environment. In order to evaluate the performance of the developed simulator, the integration tests have been conducted with the radar altimeter. Through the test, we successfully verified the performance of the simulator.

Effectiveness Analysis of Helicopter Flight Simulator and Actual Flight Training: Focused on Instrument Flight Training (헬리콥터 비행 시뮬레이터와 실 비행훈련과의 효과 분석: 계기비행 훈련을 중심으로)

  • Kim, Sang-chul;Kim, Jong-min
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.28 no.1
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    • pp.75-82
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    • 2020
  • To compare and analyze the differences between flight simulation and actual flight among 130 army helicopter pilot training subjects, the correlation analysis was performed first through t-testing and multiple regression analysis of individual characteristics and flight simulation and actual instrument flight training, which were analyzed significantly in the age (a3) and service classification (a5) of the six verification factors. This has been shown to be significant, with no difference between the flight simulator and the actual flight. Second, in order to study the correlation between aircraft types, the flight evaluation (v1) was analyzed as a dependent variable for the performance of the flight simulator (KUH: s2, UH60: s3, AH-1S: s5, UH-1H: s6), and the results of the multiple regression analysis of the flight simulator evaluation (s1) were analyzed, in contrast, as a dependent variable, and in conclusion, the training of the flight simulator provided statistical data on the possibility of replacing the actual flight training, which is thought to contribute to the orientation, budget reduction and aviation safety of the pilot training.

Simulator Development for GEO (Geostationary Orbit)-Based Launch Vehicle Flight Trajectory Prediction System (정지궤도 기반 발사체 비행 궤적 추정시스템의 시뮬레이터 개발)

  • Myung, Hwan-Chun
    • Journal of Space Technology and Applications
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    • v.2 no.2
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    • pp.67-80
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    • 2022
  • The missile early-warning satellite systems have been developed and upgraded by some space-developed nations, under the inevitable trend that the space is more strongly considered as another battle field than before. As the key function of such a satellite-based early warning system, the prediction algorithm of the missile flight trajectory is studied in the paper. In particular, the evolution computation, receiving broad attention in the artificial intelligence area, is applied to the proposed prediction method so that the global optimum-like solution is found avoiding disadvantage of the previous non-linear optimization search tools. Moreover, using the prediction simulator of the launch vehicle flight trajectory which is newly developed in C# and Python, the paper verifies the performance and the feature of the proposed algorithm.

훈련기의 종주국으로 떠오르는 한국의 항공산업

  • Lee, Hui-U
    • Defense and Technology
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    • no.5 s.255
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    • pp.18-25
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    • 2000
  • T-50은 제 3세대 훈련기의 특징을 최대한 살려서 Total Traing System으로서의 가치를 높여야 한다. 즉, 항공기 뿐만 아니라 비행시뮬레이터를 비롯한 각종 지상비행훈련장비와 정비훈련장비 등으로 Total Traing System으로서의 시너지 효과를 높이는데 주력해야 할 것이다. 또한 KT-1과 조화롭게 연계된 비행훈련체계를 구축함으로써 세계 훈련기시장에서 제 3세대 훈련기의 선두주자로서의 인식과 함께 마케팅에도 상호보완효과를 유도해 낼 수 있을 것으로 예상된다. 이제 세계 훈련기 시장의 종주국으로 거듭나고 있는 한국의 항공산업은 때마침 구조조정에 의해 새로 탄생된 한국항공우주산업(주)의 출범과 맞물려 세계 항공업계의 주목을 받기 시작했다.

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