Title of article :
An improved quaternion Gauss–Newton algorithm for attitude determination using magnetometer and accelerometer
Author/Authors :
Liu، نويسنده , , Fei and Li، نويسنده , , Jie and Wang، نويسنده , , Haifu and Liu، نويسنده , , Chang، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2014
Pages :
8
From page :
986
To page :
993
Abstract :
For the vector attitude determination, the traditional optimal algorithms which are based on quaternion estimator (QUEST) measurement noise model are complicated for just two observations. In our application, the magnetometer and accelerometer are not two comparable kinds of sensors and both are not small field-of-view sensors as well. So in this paper a new unit measurement model is derived. According to the Wahba problem, the optimal weights for each measurement are obtained by the error variance researches. Then an improved quaternion Gauss–Newton method is presented and adopted to acquire attitude. Eventually, simulation results and experimental validation employed to test the proposed method demonstrate the usefulness of the improved algorithm.
Keywords :
Attitude determination , Gauss–Newton algorithm , Magnetometer , MEASUREMENTS , Accelerometer
Journal title :
Chinese Journal of Aeronautics
Serial Year :
2014
Journal title :
Chinese Journal of Aeronautics
Record number :
2265604
Link To Document :
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