ACP-Based Space Systems: Design, Development, and Operation

Table 3

Data of orbit propagation average RMS error.

DOY	Average RMS error (m)
	Initial	1.5 h	3 h	4 h
259	7.5748	0.7400	0.7372	0.7452
260	7.3214	2.5693	1.8051	1.4724
261	6.3809	0.5543	0.4731	0.5575
262	4.4810	1.3697	0.8512	0.3074
263	2.6610	0.5866	0.4423	0.3132
264	1.4966	0.2842	0.3519	0.3983
265	2.8898	0.3763	0.3792	0.4011
266	4.4589	1.6944	1.1487	0.7630
267	6.0919	0.8121	0.7190	0.8025
268	7.8049	2.5425	1.4849	0.5297
269	7.6635	1.9015	1.2207	0.6542
270	7.1225	1.3235	1.3996	2.0675