Exponential density model - DEPRECATED
ro = CL_mod_expDensity(altitude [,prctl,h_ro])
This function is deprecated.
Replacement function: CL_mod_atmUS76
Computes the density value at a given altitude using an exponential model.
The confidence index is given by the input percentile (prctl). The other parameters of the exponential model (reference density and altitude) are function of the input altitude and prctl values.
Altitude [m]
(optional) Percentile level. Possible values are 1, 5, 33, 67, 95, 99, 100. Default is 100
(optional) Inverse of scale height (beta) [km^-1]. Default is 0.0153
Density [kg/m^3]
CNES - DCT/SB
1) ATV-CC, Technical Note, Mission analysis input data ANNEX (Time, reference frames, conventions and models for mission analysis) [DCT/SB/MS 2004-543]
2) Space Station Program Natural Environment Definition for Desing, International Space Station, Alpha (Revision B, February 8, 1994) [SSP 30425 Revision B]
altitude=[350000 360000]; [ro]=CL_mod_expDensity(altitude) [ro]=CL_mod_expDensity(altitude,67,0.0155) [ro]=CL_mod_expDensity(altitude,h_ro=0.0155) |  |  |