<< CL_kp_E2M Orbit properties CL_kp_M2E >>

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CL_kp_E2v

Eccentric anomaly to true anomaly

Calling Sequence

v = CL_kp_E2v(ecc,E)

Description

Parameters

ecc:

Eccentricity (PxN or Px1)

E:

Eccentric anomaly [rad] (PxN or Px1)

v:

True anomaly [rad] (PxN)

Authors

Bibliography

See also

Examples

// Reciprocity test
E=[3.4794 5.7281];
ecc=[0.37255 0.55];
v = CL_kp_E2v(ecc,E);
E2 = CL_kp_v2E(ecc,v);
<< CL_kp_E2M Orbit properties CL_kp_M2E >>