CL_oe_equin2kep

Description

• Converts equinoctial orbital elements to classical Keplerian orbital elements.

  The transformation jacobian is optionally computed.

  See Orbital elements for more details

Parameters

equin:

Equinoctial orbital elements [sma;ex;ey;hx;hy;L] [m,rad] (6xN)

kep:

Classical Keplerian orbital elements [sma;ecc;inc;pom;raan;anm] [m,rad] (6xN)

jacob:

(optional) Transformation jacobian (See Orbital elements for more details) (6x6xN)

Authors

• CNES - DCT/SB

See also

• CL_oe_kep2equin

• CL_oe_equin2car

Examples

// Example 1 equin = [7000.e3; -7e-3; 1e-4; 1e-4; -2e-3; 3]; kep = CL_oe_equin2kep(equin); // Example 2 equin = [7000.e3; -7e-3; 1e-4; 1e-4; -2e-3; 3]; [kep,jacob1] = CL_oe_equin2kep(equin); [equin2,jacob2] = CL_oe_kep2equin(kep); equin - equin2 // zero jacob1*jacob2 // identity