| 摘要 |
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. |
