• Title/Summary/Keyword: 헬리콥터 안전 줄 시험

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A Case Study on the Unmanned Modification Process of 500MD Helicopter (500MD 헬리콥터의 무인화 개발과정 사례 연구)

  • Kim, Won-Jin;Son, Taek-Joon;Kim, Hong-Dae;Gong, Byung-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.4
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    • pp.329-334
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    • 2021
  • Korean Air has set the goal of the first stage of the development of unmanned helicopters to perform in hovering flight by remote control. In order to achieve the development goal, Korean Air carried out system integration, ground test, and safety wire test in sequence after carrying out programmed depot maintenance and aircraft modification of manned aircraft, and verified the controllability and flight safety of the unmanned helicopter system step by step. In particular, it was confirmed that the safety wire test technique used in the final stage of verification was an effective method to verify flight safety and controllability for a fully unmanned helicopter system.

Trouble Shooting for Fully Automatic Flight Test of Small Scaled Tiltrotor UAV (축소형 틸트로터 무인기의 전자동 비행시험을 위한 문제해결과정)

  • Kang, Young-Shin;Park, Bum-Jin;Yoo, Chang-Sun;Koo, Sam-Ok;Lee, Jang-Ho
    • Aerospace Engineering and Technology
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    • v.8 no.1
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    • pp.1-9
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    • 2009
  • The ground integration test of Smart UAV has been performed according to the flight test plan. The flight test of full scaled model will be performed followed by 4 DOF ground rig test and a tethered hover test. Smart UAV is the first indigenous tiltrotor aircraft which can fly with fast cruise speed and take off or land vertically. In order to prove the flight control law of Smart UAV, the 40% scaled airplane was developed and have been tested. During flight test of small scaled model, many unique and unexpected problems occurred. After clearing these problems, fully automatic flight test was performed successfully. The experiences about many trouble shooting and resolving the problems would be basic material to avoid the unexpected but similar flight test problems hidden behind of the full scaled Smart UAV. This paper presents the detailed procedures of trouble shootings to solve the unique problems which occurred during the flight test of small scaled tiltrotor UAV.

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