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http://dx.doi.org/10.5139/JKSAS.2019.47.1.41

Alignment of Inertial Navigation Sensor and Aircraft Fuselage Using an optical 3D Coordinate Measuring Device  

Kim, Jeong-ho (Aerospace department of Pusan National University)
Lee, Dae-woo (Aerospace department of Pusan National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.47, no.1, 2019 , pp. 41-48 More about this Journal
Abstract
This paper deals with a method of aligning an aircraft fuselage and an inertial navigation sensor using three-dimensional coordinates obtained by an optical method. In order to verify the feasibility, we introduce the method to accurately align the coordinate system of the inertial navigation sensor and the aircraft reference coordinate system. It is verified through simulation that reflects the error level of the measuring device. In addition, optimization method based alignment algorithm is proposed for connection between optical sensor and inertial navigation sensor.
Keywords
Sensor Alignment; Optimization; Absolute Orientation; Inertial Navigation System; Optical Coordinate Measurement Machine;
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Times Cited By KSCI : 2  (Citation Analysis)
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