Spacecraft.StepToNode(Variable) Method |
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DescriptionSteps to the specified node of the Spacecraft's orbit based on its current central body. The next or previous node is selected based on the sign of the current propagator stepsize. If the spacecraft is already at the node, it will move off the node.
Timing Precision Mode This page describes functionality in nanosecond timing precision mode. Click here to see the documentation for this object in millisecond 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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