Spacecraft(Propagator, Ephemeris) Constructor

Top

Description

Create a Spacecraft using the first argument as the position/velocity state propagator, and second argument to propagate the attitude.

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Spacecraft(	Propagator positionPropagator,
	Ephemeris attitudeHistoryFile)

positionPropagator
Description:	The object used to propagate the Spacecraft's state
Allowed Types:	Propagator, BroadcastEphemeris, DeStateAdvancer, EarthAttitudeModel, Ephemeris, GroundHeading, GroundWaypoints, HCW, IAUIAGAttitudeAdvancer, Integrator, BulStoer, BulStoerVOP, Cowell, RK45, RK78, RK78VOP, RK89, J2Mean, KinematicAttitudeAdvancer, LunarAttitudeModel, Norad, SGP4, SpiceEphemeris, TwoBody

attitudeHistoryFile
Description:	Ephemeris object referencing an Attitude History file to use for propagating the Spacecraft's orientation

Spacecraft mySpacecraft1(myPropagator1, myEphemeris1);