Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques

Table 13

Mean pointing deviation for SCD1.

Time simulation (days)	11	8	3	2
𝜃QER	1.1553	0.8226	0.2448	0.1450
𝜃QCR	1.2003	0.8288	0.2326	0.1376
𝜃QCI	1.1306	0.8071	0.2503	0.1495