FFEccFrenet2Goals:
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Compute geometric goals given Frenet frame state and orbit info
Since version 7.
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Form:
[g,D] = FFEccFrenet2Goals( e, nu, xF, n );
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Inputs
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e (1) Eccentricity
nu (1) True anomaly [rad]
xF (6,1) Frenet frame state at nu (time-domain)
n (1) Mean orbit rate [rad/s] (optional)
* uses time-derivatives if provided
* uses nu-derivatives if NOT provided
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Outputs
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g (.) Data structure of geometric goals
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Copyright (c) 2007 Princeton Satellite Systems, Inc.
All rights reserved.
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Children:
FormationFlying: Transformation/FFEccHills2Goals
FormationFlying: Transformation/Frenet2Hills
