ViewRotatingHillsFrame:
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Animate a satellite's relative trajectory in the inertial frame.
Show the satellite traverse the relative trajectory while the trajectory
is shown rotating around the orbit path.
Since version 7.
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Usage:
h = ViewRotatingHillsFrame( rECI, vECI, rHills )
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Inputs
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rECI (3,:) Inertial position over time
vECI (3,:) Inertial velocity over time
rHills (3,:) Hills-frame position over time
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Outputs
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h (1) Handle to figure
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Children:
AeroUtils: Coord/QHills
Common: Graphics/NewFig
Common: Quaternion/QForm
Common: Quaternion/QPose
FormationFlying: Dynamics/HillsEqns
Math: Linear/Mag
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/OrbRate
SC: BasicOrbit/Period