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CL_oe_kep2cirEqua

Keplerian to circular equatorial adapted orbital elements

Calling Sequence

[cir_equa[,jacob]]=CL_oe_kep2cirEqua(kep)

Description

Parameters

kep:

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

cir_equa:

orbital elements adapted to near-circular near-equatorial orbits [sma;ex;ey;ix;iy;pom+raan+anm] [m,rad] (6xN)

jacob:

(optional) transformation jacobian d(sma,ecc,inc,pom,raan,anm)/d(sma,ex,ey,ix,iy,pom+raan+anm) (6x6xN)

Bibliography

Authors

See also

Examples

// Example 1
kep=[24464560;0.7311;0.122138;3.10686;1.00681;0.048363];
[cirequa]=CL_oe_kep2cirEqua(kep);

// Example 2
kep=[24464560;0.7311;0.122138;3.10686;1.00681;0.048363];
[cirequa,jacob1]=CL_oe_kep2cirEqua(kep);
[kep2,jacob2]=CL_oe_cirEqua2kep(cirequa);
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