#include <engine/math/numbers.hpp>
#include <cmath>
Go to the source code of this file.
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template<class T > |
T | physics::orbit::anomaly::true_to_eccentric (T ec, T ta) |
| Derives the eccentric anomaly given eccentricity and true anomaly. More...
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template<class T > |
T | physics::orbit::anomaly::true_to_mean (T ec, T ta) |
| Derives the mean anomaly given eccentricity and true anomaly. More...
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template<class T > |
T | physics::orbit::anomaly::eccentric_to_true (T ec, T ea) |
| Derives the true anomaly given eccentricity and eccentric anomaly. More...
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template<class T > |
T | physics::orbit::anomaly::eccentric_to_mean (T ec, T ea) |
| Derives the mean anomaly given eccentricity and eccentric anomaly. More...
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template<class T > |
T | physics::orbit::anomaly::mean_to_eccentric (T ec, T ma, std::size_t iterations, T tolerance) |
| Iteratively derives the eccentric anomaly given eccentricity and mean anomaly. More...
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template<class T > |
T | physics::orbit::anomaly::mean_to_true (T ec, T ma, std::size_t iterations, T tolerance) |
| Iteratively derives the true anomaly given eccentricity and mean anomaly. More...
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