Description
Sets the Spacecraft object's position and velocity at the Spacecraft's current epoch given the state vector in the specified frame and with respect to the specified origin.
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
spacecraft
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Description:
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Spacecraft whose state will be set.
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frame
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Description:
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The reference frame of the state vector.
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Valid Values:
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Value
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Label
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1
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Inertial MJ2000 Earth Equatorial
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2
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Inertial MJ2000 Ecliptic
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3
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Non-Inertial RLP Frame
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origin
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Description:
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The origin of the frame describing the state vector.
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Valid Values:
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Value
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Label
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1
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Libration Point
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2
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System Barycenter
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3
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Primary System Barycenter
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4
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Secondary System Barycenter
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posVelArray
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Description:
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The state vector containing the position and velocity which will be applied to the Spacecraft object.
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Required Size:
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6
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Syntax
myRotatingLibrationPoint1.SetSpacecraftState(mySpacecraft1, myVariable1, myVariable2, myArray1);
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See also
RotatingLibrationPoint Object
Rotating Libration Points Guide
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