Spacecraft.OrbitWizardRelativeMotionProjectedCircular(Spacecraft, Variable, Variable, Variable) Method |
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DescriptionConfigures the orbit state of the calling Spacecraft to fly in a projected circular formation with the specified separation from the primarySC. The projected circular formation causes secondarySC to revolve around the primarySC in an ellipse, where the relative trajectory forms a circle projected onto the primarySC's RIC frame Y-Z plane (i.e. the intrack-crosstrack plane). The period of the circular relative motion is the same as the orbital period of primarySC. The circular relative motion of the secondarySC is constrained to a plane that is inclined +/- 26.565 degrees from the primarySC's intrack-crosstrack plane, towards the radial direction. The user specifies the radius of the projected circle, initial phase angle, and inclination sign. An initial phase angle of zero corresponds to placing the secondarySC with an initial RIC-frame y-axis separation of zero; the z-axis separation would be at its maximum value.
This formation orbit wizard is based on the HCW system, so it assumes that the primarySC is in a two-body circular orbit, and that the secondarySC is near to the primary and propagated with the HCW propagator. If this is not the case, the actual propagated formation will not maintain the idealized relative motion.
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.
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See also Coverage and Contact Analysis Guide
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