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| int | warptwin::twoBodyPropagate (double time, double mu, clockwerk::CartesianVector< 3 > pos_initial, clockwerk::CartesianVector< 3 > vel_initial, clockwerk::CartesianVector< 3 > &pos_final, clockwerk::CartesianVector< 3 > &vel_final) |
| | Function to propagate a body between two points in time using a keplerian orbit.
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| int | warptwin::mean2eccentric (double mean_anomaly, double eccentricity, double &eccentric_anomaly, double tol, int max_iter) |
| | Function to convert mean anomaly to eccentric anomaly.
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| int | warptwin::eccentric2true (double eccentric_anomaly, double eccentricity, double &true_anomaly) |
| | Function to convert eccentric anomaly to true anomaly.
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| int | warptwin::true2eccentric (double true_anomaly, double eccentricity, double &eccentric_anomaly) |
| | Function to convert true anomaly to eccentric anomaly.
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| int | warptwin::eccentric2mean (double eccentric_anomaly, double eccentricity, double &mean_anomaly) |
| | Function to convert eccentric anomaly to mean anomaly.
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