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Дата изменения: Mon Apr 26 17:29:26 1999
Дата индексирования: Sun Mar 2 17:33:03 2014
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Creation of SPIKE / RPS2 Orbit Models

Creation of SPIKE / RPS2 Orbit Models

SPIKE currently uses constants for all orbit parameters except longitude of the ascending node (large omega). For this, SPIKE uses a linear function.

Currently we use low order fits to the 10 week ephermeridies to determine the parameters for SPIKE.

It is apparent from these plots that the rate of precession changes even now (near solar minimum) on a time scale of a year. One of the goals is to adjust the rate and constant term in our model to minimize the difference between our predicted orbital plane position and the actual position over the time span of the model.