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| Optional< Elements > | Kepler::computeOrbitalElements (const Float M, const Float mu, const Vector &r, const Vector &v) |
| | Computes the orbital elements, given position and velocity of a body. More...
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| Float | Kepler::solveKeplersEquation (const Float M, const Float e, const Size iterCnt=10) |
| | Computes the eccentric anomaly by solving the Kepler's equation. More...
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| Float | Kepler::eccentricAnomalyToTrueAnomaly (const Float u, const Float e) |
| | Computes the true anomaly from the eccentric anomaly and the eccentricity. More...
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| Float | Kepler::trueAnomalyToEccentricAnomaly (const Float v, const Float e) |
| | Computes the eccentric anomaly from the true anomaly and the eccentricity. More...
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| Vector | Kepler::position (const Float a, const Float e, const Float u) |
| | Computes the position on the elliptic trajectory. More...
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| Vector | Kepler::velocity (const Float a, const Float e, const Float u, const Float n) |
| | Computes the velocity vector on the elliptic trajectory. More...
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| Float | Kepler::meanMotion (const Float a, const Float m_total) |
| | Computes the mean motion from the Kepler's 3rd law. More...
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