| Summary: | 碩士 === 逢甲大學 === 資電碩士在職專班 === 103 === The main issue of this thesis is laser tracker and portable gage of the appearance three dimension coordinate to integrated flight control system(inertial navigate unit and flight control computer)and internal pilot camera in the Unmanned Aerial Vehicle(UAV), built internal optical measurement analysis and installation research. This method calculation the data transmission to computer, three dimension of coordinate data value can up to 0.00012in(3μm), meet the demand of flight control.
Amended by adjusting accuracy on the installation until integrated flight control system can reach its operating range (heading angle of ±0.200 degrees, pitch angle of ±0.05degrees, rolling angle of ±0.05degrees) control and flight.
On the installation of internal pilot camera measurement analysis need additional pitch angle design, mounting bracket redesign and add adjustment demands ±5.0 degrees of pitch angle.
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