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Table 1

Absolute errors between the resulting planetary orbits under the effect of single and multiple stellar impacts.

Parameters (units) Initial conditions After fourth impact After single 0.4 M impact Absolute error Accepted
a (a.u.) 40 39.9445 39.5767 0.3677 Yes
e 0 0.0171 0.0596 0.0425 Yes
i (deg) 0 0.8639 2.5511 1.6871 Yes
a (a.u.) 55 53.8292 54.3566 0.5273 Yes
e 0 0.0318 0.1683 0.1365 No
i (deg) 0 5.3190 8.2096 2.8905 Yes
a (a.u.) 69 64.1548 61.3264 2.8284 Yes
e 0 0.1015 0.1467 0.0452 Yes
i (deg) 0 2.4108 11.2228 8.8120 Yes
a (a.u.) 86 76.2692 78.7644 2.4952 Yes
e 0 0.2984 0.0597 0.2388 No
i (deg) 0 6.7236 16.6062 9.8825 Yes
a (a.u.) 98 94.6154 96.4843 1.8689 Yes
e 0 0.4955 0.4454 0.0502 Yes
i (deg) 0 14.4915 24.1467 9.6552 Yes

Notes. The reliable interval for semimajor axes is defined as 10 a.u, the reliable interval for eccentricities is defined as 0.1 and the reliable interval for inclinations is defined as 10 degrees.

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