Path: FormationFlying/Guidance
% Goals for tetrahedron geometry in an eccentric orbit.
Compute the geometric goals for a formation that achieves a tetrahedron shape
at a given true anomaly in an eccentric reference orbit.
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Usage:
g = FFEccTetrahedronGeometry( nu, d, eul );
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Inputs
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nu (1) True anomaly where tetrahedron occurs
d (1) Length of each side
eul (3,1) Euler angles defining the orientation
centroid (1) Flag. If 1, centroid of first 3 points of tetrahedron
is at the origin. Otherwise (default) the first point
is at the origin.
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Outputs
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g (.) Geometric goals data structure
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