Description
Creates a CelestialObject using the position/velocity state propagator specified by positionPropagtor, and the Attitude History file specified by ahf to propagate the attitude.
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.
Constructor Signature
Arguments
positionPropagtor
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Description:
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The object used to propagate the CelestialObject's state
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Allowed Types:
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Propagator, BroadcastEphemeris, DeStateAdvancer, EarthAttitudeModel, Ephemeris, GroundHeading, GroundWaypoints, HCW, IAUIAGAttitudeAdvancer, Integrator, BulStoer, BulStoerVOP, Cowell, RK45, RK78, RK78VOP, RK89, J2Mean, KinematicAttitudeAdvancer, LunarAttitudeModel, Norad, SGP4, SpiceEphemeris, TwoBody
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ahf
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Description:
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Ephemeris object referencing an Attitude History file to use for propagating the CelestialObject's orientation
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Allowed Types:
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Propagator, BroadcastEphemeris, DeStateAdvancer, EarthAttitudeModel, Ephemeris, GroundHeading, GroundWaypoints, HCW, IAUIAGAttitudeAdvancer, Integrator, BulStoer, BulStoerVOP, Cowell, RK45, RK78, RK78VOP, RK89, J2Mean, KinematicAttitudeAdvancer, LunarAttitudeModel, Norad, SGP4, SpiceEphemeris, TwoBody
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Syntax
CelestialObject myCelestialObject1(myPropagator1, myPropagator2);
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See also
CelestialObject Object
CelestialObjects Guide
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