Spacecraft.OrbitWizardRelativeMotionCircular(Spacecraft, Variable, Variable, Variable) Method |
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DescriptionConfigures the orbit state of the calling Spacecraft to fly in a circular formation with the specified separation from the primarySC. The circular formation causes the secondarySC to revolve around the primary at a constant distance. The period of the circular relative motion is the same as the orbital period of the primarySC. The circular relative motion of the secondarySC is constrained to a plane that is inclined +/- 30 degrees from primarySC's intrack-crosstrack plane, towards the radial direction. The user specifies the circular formation radius, 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 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. Click here to see the documentation for this object in nanosecond timing precision mode.
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See also Coverage and Contact Analysis Guide
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