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CL_kp_v2E

True anomaly to eccentric anomaly

Calling Sequence

E = CL_kp_v2E(ecc,v)

Description

Parameters

v:

True anomaly [rad] (PxN or Px1)

ecc:

Eccentricity (PxN or Px1)

E:

Eccentric anomaly. Undefined (%nan) if the true anomaly is not in the correct range. [rad] (PxN)

Authors

Bibliography

See also

Examples

// consistency test
v=[3.4794 5.7281];
ecc=[0.37255 0.55];
E = CL_kp_v2E(ecc,v);
v2 = CL_kp_E2v(ecc,E);
<< CL_kp_params Orbit properties CL_kp_v2M >>