Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques

Table 10

Mean deviations for different time simulation for declination and right ascension and SCD2 (in degrees).

Time Simulation (days)	12	8	5	2
𝛼SCC−𝛼QER	−0.1266	−0.0200	0.0180	0.0100
𝛼SCC−𝛼QCR	−0.1334	−0.0247	−0.0153	−0.0093
𝛼SCC−𝛼QCI	−0.1875	−0.0565	−0.0139	0.0065
𝛿𝛼SCC−𝛿𝛼QER	−0.1358	−0.0925	−0.0520	−0.0099
𝛿SCC−𝛿QCR	−0.1312	−0.0894	−0.0502	−0.0096
𝛿SCC−𝛿QCI	−0.1925	−0.1397	−0.1088	−0.0210