Predicting IGS RTS Corrections Using ARMA Neural Networks

Table 2

Prediction RMS errors for five days (January 6 to January 10, 2015).

Day number	3D orbit (m)			Clock (m)			Ap	F10.7
	Polynomial	ARMA	ARMANN	Polynomial	ARMA	ARMANN
6	0.552	0.055	0.046	2.234	0.068	0.057	13	142
7	0.982	0.058	0.054	2.811	0.096	0.092	38	147
8	0.697	0.056	0.051	2.605	0.081	0.081	16	157
9	0.572	0.037	0.036	2.072	0.059	0.055	8	151
10	0.601	0.043	0.039	2.905	0.059	0.057	10	152
Mean	0.681	0.050	0.046	2.526	0.073	0.068	17	150
STD	0.177	0.009	0.008	0.362	0.016	0.017	12	6