Spacecraft.StepToApsis(Variable) Method |
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DescriptionSteps to the specified apsis of the Spacecraft's orbit based on its current central body. The next or previous apsis is selected based on the sign of the current propagator stepsize.
Timing Precision Mode This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode. Click here to see the documentation for this object in nanosecond timing precision mode.
Method Signature
Arguments
Return Value
Returns the duration of the total step taken.
Syntax
See also Coverage and Contact Analysis Guide
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