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celestlab >> DEPRECATED > CL_mod_expDensityDrag

CL_mod_expDensityDrag

Atmospheric drag using exponential density model - DEPRECATED

Calling Sequence

acc = CL_mod_expDensityDrag(altitude, cbal [, er, mu])

Description

Parameters

altitude :

Satellite's altitude. [m] (1xN)

cbal :

Satellite's ballistic coefficient : S*cx/m with S=equivalent drag surface, cx = drag coefficient, m = mass. [m^2/kg](1xN)

er:

(optional) Equatorial radius. Default: %CL_eqRad. [m] (1x1)

mu:

(optional) Gravitational constant. Default: %CL_mu. [m^3/s^2] (1x1)

acc:

Drag acceleration. [m/s^2] (1xN)

Authors

See also

Bibliography

Examples

[acc] = CL_mod_expDensityDrag([350000, 360000, 350000, 360000],[2.2, 2.3, 2.3, 2.2])

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