.....

     - default

   * - V0

     - input

     -

     - float

     - velocity at launch

     - 0-10000

     - 600

   * - sigma_V0

     - input

     -

     - float

     - error on velocity at launch

     - 0-500

     - 50

   * - Time_UTC

     - input

     -

     - datetime

     - t0, datetime of start date

     -

     -

   * - sigma_t0

     - input

     -

     - float

     - error on start date

     - 0-10000

     - 3000

   * - Rs

     - input

     -

     - float

     - distance from the Sun at t0 in R_sun

     - 0-50

     - 21.5

   * - dRs

     - input

     -

     - error on t0

     - float

     - error on Rs

     - 0-10

     - 1

   * - Target

     - configuration

     -

     - str

     - Propagation Target

     -

     - Earth

   * - W

     - input

     -

     - solar wind average veolcity

     - 420600

     - float

     - solar wind average velocity

     - 420,600

     - 420

   * - sigma_W

     - input

     -

     - float

     - solar wind velocity standard devistion

     - 50,66

     - 50

   * - gammaPDF

     - configuration

     -

     - str

     - Type of PDF for Gamma

     - NORMAL, LOGNORMAL, SWEPT

     - LOGNORMAL

   * - Omega

   * - Phi_CME

     - input

     - float

     - Central meridian distance in degrees 

     - -90-90

     -

     - Carrington Latitudeof the ICME main vector

     - 0-360

     -

   * - Sigma_Omega

   * - Sigma_Phi_CME

     - input

     -

     - Error on the latitude

     - float

     - Error on Phi

     - 0-60

     - 5

   * - Phi_CME

   * - Omega

     - input

     -

     - Width of the ICME

     - 10-360

     - float

     - Half width of the ICME

     - 10-180

     - 60

   * - Sigma_Phi_CME

   * - Sigma_Omega

     - input

     -

     - float

     - Error on the the Width of the ICME

     - 0-60

     - 5