The present invention relates to an on-board measurement method using an on-board measurement system optimized for properties of an aircraft and a test purpose and, more specifically, to an on-board measurement method using an on-board measurement system optimized for properties of an aircraft and a test purpose characterized by including: a first step (S100) of designing the on-board measurement system in accordance with measurement requirements to design and analyze the aircraft defined by conceptual design and preliminary design of an aircraft development process and to verify functions of each system; a second step (S200) of selecting measurement sensors in accordance with a parameter desired to measure by critical design of the aircraft development process and properties of the parameter, mounting the on-board measurement system designed in the first step (S100), and determining the normal operation of the measurement sensors; and a third step (S300) of acquiring flight data when the normal operation of the measurement sensors are verified through the second step (S200) by performing a test & evaluation of the aircraft manufactured in a trial manufacture step of the aircraft development process by using the on-board measurement system. The purpose of the present invention is to provide the on-board measurement method using the on-board measurement system optimized for the properties of the aircraft and the test purpose capable of conveniently acquiring various information about the aircraft by using the on-board measurement system optimized for the properties of the aircraft and the test purpose.

    본 발명은 항공기 특성과 비행 시험 목적에 최적화된 탑재계측 시스템을 이용한 탑재계측 방법에 관한 것으로, 더욱 상세하게는 항공기 개발 과정의 개념설계(Conceptual Design) 및 기본설계(Preliminary Design)에 의해 정의된 개발 항공기의 설계 및 해석, 각 계통별 기능을 검증하기 위한 계측요구도에 따라, 탑재계측 시스템 설계를 수행하는 제 1 단계(S100), 항공기 개발 과정의 상세설계(Critical Design)에 의해 측정하고자 하는 파라미터 및 파라미터 특성에 따라 계측센서를 선정하며, 상기 제 1 단계(S100)에 의해 설계된 탑재계측 시스템을 장착하고 계측센서들의 정상 작동 여부를 판단하는 제 2 단계(S200) 및 상기 제 2 단계(S200)에 의해, 계측센서들의 정상 작동 상태를 확인될 경우, 탑재계측 시스템을 이용하여 항공기 개발 과정의 시제작(Manufacture)에서 제작된 개발 항공기의 시험평가(Test & Evaluation)를 수행하여 비행 데이터를 획득하는 제 3 단계(S300)로 이루어지는 것을 특징으로 하는 항공기 특성과 비행 시험 목적에 최적화된 탑재계측 시스템을 이용한 탑재계측 방법에 관한 것이다.


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    Title :

    ONBOARD FLIGHT TEST OPTIMIZED AIRCRAFT CHARACTER AND OBJECT OF TESTING FLIGHT


    Additional title:

    항공기 특성과 비행 시험 목적에 최적화한 탑재계측 시스템을 이용한 탑재계측 방법


    Contributors:

    Publication date :

    2016-04-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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