Title : 
Analysis of the residual between the model and the data using autocorrelation function for satellite attitude estimation
         
        
            Author : 
Hamzah, N.H. ; Yaacob, Sazali ; Muthusamy, H. ; Hamzah, N.
         
        
            Author_Institution : 
Sch. of Mechatron. Eng., Univ. Malaysia Perlis, Arau, Malaysia
         
        
        
        
        
        
            Abstract : 
Objective of this paper is to investigate whether the noise in attitude dynamics model and measurement model is Gaussian white noise process or not. This is important because if the assumption regarding the noise is wrong, this will lead to unreliable and inaccurate estimation. The residual between the standard model and the real data is computed and is analyzed using autocorrelation function via Minitab software. The result shows that the error in the attitude dynamics model is not Gaussian white noise, while the error in measurement model is Gaussian white noise.
         
        
            Keywords : 
AWGN; aerospace computing; artificial satellites; attitude measurement; computerised instrumentation; correlation methods; measurement errors; Gaussian white noise process; Minitab software; attitude dynamics model; autocorrelation function; measurement error model; residual analysis; satellite attitude estimation; Correlation; Data models; Estimation; Mathematical model; Noise measurement; White noise; Satellite attitude estimation; autocorrelation function; noise;
         
        
        
        
            Conference_Titel : 
Signal Processing and its Applications (CSPA), 2013 IEEE 9th International Colloquium on
         
        
            Conference_Location : 
Kuala Lumpur
         
        
            Print_ISBN : 
978-1-4673-5608-4
         
        
        
            DOI : 
10.1109/CSPA.2013.6530018