Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques

Table 8

INPE’s Satellite Control Center Data (index SCC) and computed results with the satellite in circular orbit and under the influence of the residual magnetic torque (index QCR) for declination and right ascension and SCD2 (in degrees).

Day	𝛼SCC	𝛼QCR	𝛼SCC−𝛼QCR	𝛿SCC	𝛿QCR	𝛿SCC−𝛿QCR
12/02/02	278.71	278.710000	0	63.47	63.470000	0
13/02/02	278.73	278.7113	0.01870	63.45	63.4692	−0.0192
14/02/02	278.74	278.7127	0.02733	63.42	63.4683	−0.0482
15/02/02	278.74	278.7141	0.0259	63.39	63.4673	−0.0773
16/02/02	278.72	278.7155	0.0045	63.36	63.4664	−0.1064
17/02/02	278.68	278.7168	−0.0368	63.33	63.4654	−0.1354
18/02/02	278.63	278.7180	−0.0880	63.31	63.4646	−0.1546
19/02/02	278.57	278.7191	−0.1491	63.29	63.4638	−0.1738
20/02/02	278.50	278.7200	−0.2200	63.27	63.4631	−0.1931
21/02/02	278.42	278.7207	−0.3007	63.25	63.4625	−0.2125
22/02/02	278.33	278.7212	−0.3913	63.24	63.4621	−0.2221
23/02/02	278.23	278.7215	−0.4916	63.23	63.4618	−0.2318