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I have been testing different methods for defining the Earth's gravity effect on a spacecraft:
According to the documentation, both methods should yield the same results, as they are equivalent. However, after a short propagation, I observe divergent results. Specifically, with gravModel == 2 I obtain osculating orbital elements.
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Hello everyone,
I have been testing different methods for defining the Earth's gravity effect on a spacecraft:
According to the documentation, both methods should yield the same results, as they are equivalent. However, after a short propagation, I observe divergent results. Specifically, with
gravModel == 2
I obtain osculating orbital elements.Does anyone know why this discrepancy occurs?
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