Research Article
A Note on the Use of Generalized Sundman Anomalies in the Numerical Integration of the Elliptical Orbital Motion
Table 1
Errors in position and velocity for HEOS I in
and
, respectively.
| | | | | | |
| 0.0 | 953553.59323 | 770880.33913 | 1.6 | 0.00086 | 0.00078 | 0.1 | 258032.45040 | 208605.19468 | 1.7 | 0.00037 | 0.00037 | 0.2 | 66193.91357 | 53516.13695 | 1.8 | 0.00016 | 0.00020 | 0.3 | 16522.81621 | 13359.02237 | 1.9 | 0.00005 | 0.00011 | 0.4 | 4074.21292 | 3294.34188 | 2.0 | 0.00009 | 0.00003 | 0.5 | 1002.70466 | 810.86164 | 2.1 | 0.00032 | 0.00030 | 0.6 | 248.26083 | 200.79429 | 2.2 | 0.00112 | 0.00127 | 0.7 | 62.24464 | 50.35530 | 2.3 | 0.00320 | 0.00399 | 0.8 | 15.89750 | 12.86526 | 2.4 | 0.00961 | 0.01251 | 0.9 | 4.15863 | 3.36714 | 2.5 | 0.03029 | 0.03987 | 1.0 | 1.12001 | 0.90756 | 2.6 | 0.10106 | 0.13113 | 1.1 | 0.31248 | 0.25354 | 2.7 | 0.36030 | 0.45054 | 1.2 | 0.08991 | 0.07312 | 2.8 | 1.37345 | 1.62725 | 1.3 | 0.02677 | 0.02188 | 2.9 | 5.59493 | 6.21512 | 1.4 | 0.00880 | 0.00725 | 3.0 | 24.23229 | 25.17338 | 1.5 | 0.00282 | 0.00238 | 3.1 | 110.62982 | 107.96944 |
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