RelativeMotionUtilities.ComputeStateHCW(Array, Variable, TimeSpan, Variable, Variable) Method |
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DescriptionPredicts a future position and velocity by evaluating the HCW equations using the specified primary satellite mean motion, relative state vector of the secondary satellite in units of km and km/s, and time interval deltaT. This overload assumes the Earth is the central body. The inputOutputSystem argument specifies the coordinate system of both the input and output relative states. The coordinateSetToPropagate argument is used to specify whether the HCW equations of motion are propagated using the Cartesian, RIC Cylindrical, or RIC Spherical relative state vector. The output state will be returned in units of km and km/s
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 predicted future position and velocity of a secondary Spacecraft.
Syntax
See also RelativeMotionUtilities Object RelativeMotionUtilities.ComputeStateHCW
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