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Path: Orbit/OrbitCoord
% Computes the orbit velocity in the perifocal plane.
Since version 1.
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Form:
vPQ = VPQ( e, p, nu, mu )
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Inputs
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e Eccentricity
p The parameter
nu (:) True anomaly (rad)
mu Gravitational parameter
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Outputs
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vPQ (3,:) Velocity
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References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988,
pp. 63-64.
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Common: Graphics/Plot2D
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