Examples
// Mean anomaly to true anomaly : ecc = 0.3; M = [-0.1, 10.2]; // rad v = CL_kp_anomConvert("M", "v", ecc, M) // Consistency test: M - CL_kp_anomConvert("v", "M", ecc, v) // => 0 |  |  |
Conversion of anomaly
[anom2] = CL_kp_anomConvert(type_anom1, type_anom2, ecc, anom1)
Converts anomaly from one type to another.
Available types are:
- "M" : mean anomaly
- "v" : true anomaly
- "E" : eccentric anomaly
Elliptic and hyperbolic orbits are supported.
See Orbital elements for more details on orbital elements.
(string) Type of input anomaly ("M", "E", "v") (1x1)
(string) Type of output anomaly ("M", "E", "v") (1x1)
Eccentricity (1xN or 1x1)
Input anomaly of type type_anom1 (1xN or 1x1)
Output anomaly of type type_anom2 (1xN)
CNES - DCT/SB
// Mean anomaly to true anomaly : ecc = 0.3; M = [-0.1, 10.2]; // rad v = CL_kp_anomConvert("M", "v", ecc, M) // Consistency test: M - CL_kp_anomConvert("v", "M", ecc, v) // => 0 | | |