• Title, Summary, Keyword: Training Aircraft

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A Development of 3D video simulation system using GPS (GPS와 9-axis sensor를 이용한 3D 영상 구현 시뮬레이션 시스템)

  • Joo, Sang-Woong;Shim, Kyou-Chul;Kim, Kyeong-Hwan;Zhu, Jiang;Liu, Hao;Liu, Jie;Jeong, Hoe-Kyung
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • pp.1021-1023
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    • 2013
  • Currently, aircraft and automobile simulator for training provides a variety of training by making hypothetical situation on a simulator Installed on the ground Currently. And the instructor maximizes the effectiveness of the training by Monitoring training and instructing the required training. When trainees are boarding the aircraft or automobile. The Instructor in the ground is not able to monitoring aircraft, automobile. The assessment of the training is not easy after the end of the training Therefore, it is difficult to provide high quality of education to the students. In this paper, Simulation software is to develop the following. Collecting GPS and real-time information for aircraft, automobile ${\grave{a}}implementing$ 3D simulation. Implementing Current image of the aircraft or automobile in the screen by 3D Real-time monitoring of training situation at the control center utilizing for training saving 3D video files Analysis, evaluation on training After the end of the training.

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Estimation and Validation of Longitudinal Stability/Control Derivatives for the Flight Training Device of a Light Aircraft

  • Lee, Jung Hoon
    • International Journal of Aerospace System Engineering
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    • v.5 no.1
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    • pp.9-18
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    • 2018
  • The longitudinal flight parameters of a light airplane are estimated from flight test data by use of the output error method. The reliability of the flight test measurement is examined in engineering judgment, scatter and Cramer-Rao bound, which turns out to be satisfactory with minor defects. Estimated parameter values are validated by comparing the simulated responses with the ones from actual flight tests. The FTD(Flight Training Device) of a light airplane turns out to satisfy the qualification of FAA Level 5 FTD in longitudinal motion. All the necessary practices for generation of high-fidelity data in longitudinal motion of a light aircraft are successfully performed in this study.

Noise Analysis of Turbo Prop Aircraft(C90GT) (터보프롭 항공기(C90GT)의 소음 분석)

  • Ryu, Jong-Hyeon;Kim, Woo-Jin;Kim, Gyou-Beom
    • Journal of Convergence for Information Technology
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    • v.9 no.9
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    • pp.141-146
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    • 2019
  • The aircraft noise analysis area in this study is a training airfield where various kinds of aircraft are operated. It is difficult to identify the noise analysis as a real measurement in a training airfield. In order to overcome these practical limitations and to establish appropriate noise countermeasures, a noise map is prepared using the Integrated Noise Model Version 7.0 of the aircraft noise prediction program used by the FAA. The noise of C90GT aircraft was measured while flying the takeoff route, landing route, and long route. We want to identify areas where noise damage is more than 70 WECPNL. No area exceeding the legal standard of 70 WECPNL was found in all routes.

Development of Aircraft and Radar Simulation for Air Traffic Control Training System (항공관제 훈련용 항공기 및 레이더 시뮬레이션 시스템 구축)

  • Oh, Hye-Ju;Cho, Sang-Ook;Choi, Keeyoung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.4
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    • pp.305-313
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    • 2013
  • This paper presents a simulation system for air traffic control (ATC) training. The structure of the ATC is analyzed to define simulation components to be developed. Requirements that must be satisfied by a training simulator are also identified. The results were reflected in the design of the simulator. The training simulator is composed of three modules same as in real life : air traffic controller, aircraft, radar. Each developed module performs the strict unit tests and combine test based on the scalability, ease, real-time, the operating range of the algorithm derived from the requirements. The simulation system can be connected to an actual ATC, and used to validate the ATC system. At peak load, 1200 aircraft and 30 radars can be operated simultaneously.

Requirements and Considerations for Qualification and Training of RPA Pilot (무인항공기 조종사 자격/교육훈련 요구사항 및 고려사항)

  • Hwang, You-Chul;Kang, Ja-Young
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.1
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    • pp.74-79
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    • 2013
  • Early remotely-piloted aircraft system (RPAS) development focused on simple reconnaissance to obtain information by visual observation for military demands. Currently, various types of remotely-piloted aircraft (RPA) is being developed worldwide for applications in many different areas. As RPA avionics are combined with CNS/ATM technologies, RPA capabilities will be enhanced and the market is expected to grow rapidly. ICAO has been held the Air Navigation Commission on 14 October 2011 to discuss revising Procedures for air navigation services (PANS) and guidance material related to RPA and their associated systems. It progressed that Annex 2 and 7 will be revised and came into effect from 2012. However most of incorporate revisions are not clear yet. Because the revision articles recommend follow requirements of the state(s). Considering operations of RPA in controlled airspace and between adjacent states, the qualification and training of RPA pilot will be one of the main issues for RPA operation. In this paper, we will take a look at international and domestic trends of regulation framework in ICAO and RPA advanced country in chapter 2.1 and suggest about consideration of remote pilot qualification and training for establishing regulations of remote pilot license.

Training and Performances of the HPA Pilot (인간동력항공기 조종사 훈련 및 성과)

  • Chang, Sang-Hyun;Lee, Jeong-Won
    • Aerospace Engineering and Technology
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    • v.12 no.2
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    • pp.202-208
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    • 2013
  • This paper describes establishment of a pilot training plan, training and an outcome for Human Powered Aircraft which can take off, landing and fly using the energy generated by only human muscle without using mechanical power. To achieve these, a special trainer made a plan by considering physical trait of each pilot and each pilot was performed an indoor training for principle physical improvement, an outdoor training for generating sustainable power, a simulation training to learn maneuver ability. The pilot mastered the basic maneuver ability needed to fly and each pilot was lose their weight and experienced their improved physical strength via the training.

Study on How to Maintain the Flight Test Currency of Certification Flight Test Crew (항공기 인증비행시험요원의 비행시험 자격 유지 방안 연구)

  • Kee, Yeho
    • Journal of Aerospace System Engineering
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    • v.7 no.3
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    • pp.45-50
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    • 2013
  • This is a research report about the method of how to maintain qualification of certification flight test crews. KCA(Korea Certification Agency) have completed the KC-100 airplane certification flight tests which is the first time experienced flight tests operation. After the certification flight test, it has been found that annual flying time requirement of 100 hours to the certification flight test pilot is too strict, and other several requirements to maintain the qualification of the certification test crew such as aircraft certification introduction training, initial flight test pilot and flight test engineer certification training, crew resource management training, aviation physiology training, and survival training was difficult to implement in Korean civil aviation environments. In this study, it was suggested that 30 hours of flying time for maintaining certification flight test pilot qualification could be applied to contribute for safe operation of certification flight test and the other training requirements of the certification flight test crew could be fulfilled using self made training courses, existing FAA training courses and Korean Air Force training resources. Therefore, it is recommended that the regulation of maintaining the certification flight test crew qualification should be refined to implement the requirement practically.

Roles of Safety Management System (SMS) in Aircraft Development

  • Lee, Won Kwan;Kim, Seung Jo
    • International Journal of Aeronautical and Space Sciences
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    • v.16 no.3
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    • pp.451-462
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    • 2015
  • Safety is the first priority in civil aviation, and so the International Civil Aviation Organization (ICAO) has introduced and mandated the use of Safety Management Systems (SMS) by airlines, airports, air traffic services, aircraft maintenance organizations, and training organizations. The aircraft manufacturing industry is the last for which ICAO has mandated the implementation of SMS. Since SMS is a somewhat newer approach for most manufacturers in the aviation industry, they hardly believe in the value of implementing SMS. The management of safety risk characteristics that occur during early aircraft development stages and the systematic linkage that the safety risk has to do with an aircraft in service could have a significant influence on the safe operation and life cycle of the aircraft. This paper conducts a case analysis of the McDonnell Douglas MD-11 accident/incident to identify the root causes and safety risk levels, and also verified why aircraft manufacturing industry should begin to adopt SMS in order to prevent aircraft accident.

THE IMPACT OF AIRCRAFT NOISE ON MILITARY EXERCISE AND TRAINING AREAS

  • Bugge, Jens-Jorgen;Knut Fuglum, Bjorn Tronstad
    • Proceedings of the Acoustical Society of Korea Conference
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    • pp.812-816
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    • 1994
  • Gardermoen is chosen as the location for a new major airport for the Oslo area, The site is surrounded by various units and camps operated by the Norwegian national defence. A study was carried out to evaluate whether the occurrence of aircraft noise may result in the national defence having to restrict operations in established camps, and in areas where outdoor exercise, training and instruction are beeing carried out.

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Aircraft Identification and Orientation Estimention Using Multi-Layer Neural Network (다층 신경망을 사용한 항공기 인식 및 3차원 방향 추정)

  • Kim, Dae-Young;Chien, Sung-Il;Son, Hyon
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.16 no.1
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    • pp.35-45
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    • 1991
  • Multi layer neural network using backpropagation learning algorithm is used to achieve identification and orientation estimation of different classes of aircraft in the variety of 3-D orientations. In-plane distortion invarient$(L,\;{\Phi})$ feature was extracted from each aircraft image to be used for training neural network aircraft classifier. For aircraft identification the optimum structure of the neural network classifier is studied to obtain high classification performance. Effective reductioin of learning time was achieved by using modified backpropagation learning algorithm and varying, learning parameters.

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