Aircraft Attitude Determination Method Based on GNSS
LIU Shuai
ZHAO Guorong
WANG Yuanxin
CAO Weiyi
Abstract：This paper mainly studies on the attitude determination of aircraft based on GNSS. Considering the fact that the baseline of attitude determination system is fixed,the carrier phase single difference equation is build to compute the attitude. A method based on the robust kalman filtering is presented to solve the problem of gross error in measurement data. The simulation re?sult shows that the precision and reliability of the presented method is better than the least squares method.
Keywords：attitude determinationcarrier phase single difference equationrobust kalman filtering
Publication Date：2017-01-01
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：4( 1077-1080 )