Attitude model identification of on-orbit satellites

摘要

Having filtered the whole data by WD technology, it is now straightforward to apply the general recursive prediction error algorithm to the BJM in equation (5) to obtain the GAM and its related noise model ([12] [Ljung] and Söderström, 1983): Equation 12 [Figure omitted. See Article Image.] Equation 13 [Figure omitted. See Article Image.] Equation 14 [Figure omitted. See Article Image.] Equation 15 [Figure omitted. See Article Image.] Equation 16 [Figure omitted. See Article Image.]