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CL_kp_M2E

Mean anomaly to eccentric anomaly (Kepler's equation)

Calling Sequence

E = CL_kp_M2E(ecc,M)

Description

Parameters

M:

Mean anomaly [rad] (PxN or Px1)

ecc:

Eccentricity (PxN or Px1)

E:

Eccentric anomaly [rad] (PxN)

Authors

Bibliography

See also

Examples

E = CL_kp_M2E(0.001,3*%pi/8) // elliptical orbit
E = CL_kp_M2E(1.1,3*%pi/8) // hyperbolic orbit
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