• 제목/요약/키워드: tower fly By method

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비행시험을 통한 경비행기의 속도계 보정에 대한 연구 (Airspeed and Altitude Calibration of Light Airplane via Flight Test)

  • 이정훈;김성훈
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.891-896
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    • 2007
  • This paper contained the flight test calibration for the airspeed indicator and the altimeter of the light airplane ChangGong-91, which is the first type certified aircraft from Korean Ministry of Construction and Transportation, as a part of the flight test validation. The flight test for airspeed position error calibration was performed using tower fly by method in order to calibrate swivel head testboom which is attached to the right wing tip of the airplane, and using system to system method for airspeed indicator. The altimeter calibration was calculated using flight test data for airspeed calibration. The flight test was conducted at the basis of the 'Korean Airworthiness Standard' regulation of Korean Ministry of Construction and Transportation.

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비행시험을 통한 경비행기의 속도계 보정 (Airspeed Calibration of a Light Airplane via Flight Test)

  • 이정훈;류시융;이장호
    • 제어로봇시스템학회논문지
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    • 제14권7호
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    • pp.629-634
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    • 2008
  • This paper presents the flight test procedure and the results for the airspeed indicator calibration of a light airplane the name of ChangGong-91, which is the first type certified aircraft from Korean Ministry of Construction and Transportation, as a part of the flight test validation to get the certification. The flight tests for airspeed position error calibrations are conducted using tower fly by method in order to calibrate swivel head testboom which is attached to the right wing tip of the airplane. Also system to system method is applied in order to calibrate the airspeed indicator of the cockpit. The flight test is conducted at the basis of the 'Korean Airworthiness Standard' which is the regulation of Korean Ministry of Construction and Transportation. The airspeed error range for the testboom and the airspeed indicator are determined to $-0.75{\sim}+0.75$ knot and to $-4.0{\sim}+2.0$ knots, respectively. The calibration results are applied to ChangGong-91 Flight Operation Manual.

슬립폼 적용을 위한 고강도콘크리트의 조기강도 발현성상에 관한 실험적 연구 (An Experimental Study on Early Strength Development of High-Strength Concrete to Apply Slip-Form)

  • 주지현;여동구;강석표;길배수;남재현;김무한
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2000년도 가을 학술발표회논문집(I)
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    • pp.355-358
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    • 2000
  • Nowadays, with high-storied and large-sized of structures, high-strength concrete is applied to the various kinds of concrete structure. Among of them, for reduction of completion time, high-strength concrete is applied to the high-storied tower, building which is constructed continuously by the slip-form method and it is expected to be on the increase. In this case, it is very important to grasp development of early-strength to apply the slip-form method. But the strength data prior 1 day is rare. Therefore, to apply slip-form method in field, this study aim is to present basic data for development of early-strength of high-strength concrete, through examining development of strength by different curing temperature, replacement of fly-ash.

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소형 항공기 개발 동정압계통 오차 확인 비행시험 사례 (Study on Flight Test Practice of the Small Civil Airplane Development for Pitot-Static System's Error Identification)

  • 김찬조;서지한;이원중
    • 항공우주시스템공학회지
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    • 제7권3호
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    • pp.33-38
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    • 2013
  • The air data measured from the static pressure, the dynamic pressure and etc. of an airplane is used for calculation of many flight parameters(altitude and airspeed and so on) and these values applied to flight safety and navigation flight. The pitot-static system of the development airplane is calibrated by finding of pitot-static system's error using tower fly-by, trailing cone method and etc. This paper is describing for the introduction of the trailing cone method and major items for test planning, preparation, operation and results for air data calibration flight test performed, considering efficiency and safety during KC-100 development project.