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CelestLab >> DEPRECATED > CL_fr_J20002G50

CL_fr_J20002G50

EME2000 (J2000) to Gamma50 (Veis) vector transformation - DEPRECATED

Calling Sequence

[pos_G50,vel_G50,jacob] = CL_fr_J20002G50(cjd,pos_J2000 [,vel_J2000,dPsi,dEps,conv_iers])

Description

Parameters

cjd:

modified julian day from 1950.0 (UTC) (1xN or 1x1)

pos_J2000:

position vector relative to EME2000 [m] (3xN or 3x1)

vel_J2000:

(optional) velocity vector relative to EME2000 [m/s] (3xN or 3x1)

dPsi :

(optional) Nutation corrections [radians] (default is 0) (1xN or 1x1)

dEps :

(optional) Nutation corrections [radians] (default is 0) (1xN or 1x1)

conv_iers :

(optional) Convention IERS. Only IERS 1996 (Lieske/Wahr) is implemented (default is "iers_1996")

pos_G50:

position vector relative to Gamma50 (Veis) [m] (3xN)

vel_G50:

(optional) velocity vector relative to Gamma50 (Veis) [m/s] (3xN)

jacob:

(optional) jacobian of the transformation (6x6xN)

Authors

Bibliography

See also

Examples

// Conversion of position J2000 to G50
pos_J2000=[[3500.e3;2500.e3;5800.e3] , [4500.e3;2100.e3;6800.e3]];
cjd = [21010 , 21011];
pos_G50=CL_fr_J20002G50(cjd,pos_J2000);

// Conversion of position and velocity : J2000 to G50  + jacobian
pos_J2000=[[3500.e3;2500.e3;5800.e3] , [4500.e3;2100.e3;6800.e3]];
vel_J2000 = [ [1.e3;3.e3;7.e3] , [1.e3;3.e3;7.e3]];
cjd = [21010 , 21011];
[pos_G50,vel_G50,jacob]=CL_fr_J20002G50(cjd,pos_J2000,vel_J2000);

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