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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/BasicOrbit
% Compute the period for any orbit.
You can specify a semi-major axis or a Cartesian position. The default
central body is the Earth.
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Form:
p = Period( a, mu )
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Inputs
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a (1,1) or (6,1) Semi-major axis (is inf for a parabola and -
for a hyperbola) or [x;y;z;vX;vY;vZ]
mu (1,1) Gravitational parameter (default = 3.98600436e5)
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Outputs
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p (1,1) Period
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Common: Graphics/Plot2D SC: BasicOrbit/RV2El
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