Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques

Table 4

Mean deviations for different time simulations for declination and right ascension and SCD1 (in degrees).

Time Simulation (days)	11	8	3	2
𝛼SCC−𝛼QER	−1.5882	−0.5435	0.2566	−0.0151
𝛼SCC−𝛼QCR	−1.0779	−0.3587	0.2444	−0.0258
𝛼SCC−𝛼QCI	−1.5400	−0.5047	0.2710	0.0074
𝛿𝛼SCC−𝛿𝛼QER	−1.0896	−0.8034	−0.2364	−0.1449
𝛿SCC−𝛿QCR	−1.1707	−0.8172	−0.2241	−0.1376
𝛿SCC−𝛿QCI	−1.0653	−0.7882	−0.2416	−0.1495