pdbmodel added

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UNITOV P-DBM CME propagation model

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.. contents:: Table of contents

The CME propagation is modeled by using probability distribution functions. This allows us to evaluate the ICME arrival times and velocities along with the uncertainties  on the forecast.

References

~~~~~~~~~~

https://doi.org/10.1051/swsc/2018003

Model summary

~~~~~~~~~~~~~

.. list-table::

  * - **internal_name:**

    - unitov_pdb_model

  * - **publisher:**

    - University of Rome Tor Vergata

  * - **alph_code:**

    - 39A

  * - **id_tmp:**

    - xx

  * - **identifier:**

    - aspis:///unitov/pdb_model

  * - **type:**

    - software

  * - **language:**

    - Python 3.x

  * - **dependencies:**

    - numpy, matplotlib, ephem, astroquery, datetime, sunpy

  * - **latest update:**

    - 2023-11-10 12:45:00

Parameters

~~~~~~~~~~

.. list-table:: 

   :widths: 15 15 10 30 15 15

   :align: right 

   :header-rows: 1

   * - name

     - scope

     - type

     - description

     - domain

     - default

   * - V0

     - input

     -

     - velocity at launch

     - 0-10000

     - 600

   * - sigma_V0

     - input

     -

     - error on velocity at launch

     - 0-500

     - 50

   * - Time_UTC

     - input

     -

     - t0, datetime of start date

     -

     -

   * - sigma_t0

     - input

     -

     - error on start date

     - 0-10000

     - 3000

   * - Rs

     - input

     -

     - distance from the Sun at t0 in R_sun

     - 0-50

     - 21.5

   * - dRs

     - input

     -

     - error on t0

     - 0-10

     - 1

   * - Target

     - configuration

     -

     - Propagation Target

     -

     - Earth

   * - W

     - input

     -

     - solar wind average veolcity

     - 420600

     - 420

   * - sigma_W

     - input

     -

     - solar wind velocity standard devistion

     - 50,66

     - 50

   * - gammaPDF

     - configuration

     -

     - Type of PDF for Gamma

     - NORMAL, LOGNORMAL, SWEPT

     - LOGNORMAL

   * - Omega

     - input

     -

     - Carrington Latitudeof the ICME main vector

     - 0-360

     -

   * - Sigma_Omega

     - input

     -

     - Error on the latitude

     - 0-60

     - 5

   * - Phi_CME

     - input

     -

     - Width of the ICME

     - 10-360

     - 60

   * - Sigma_Phi_CME

     - input

     -

     - Error on the the Width of the ICME

     - 0-60

     - 5

   * - CME

     - output

     - PNG image

     - Visualization of the ICME propagation

     -

     -

   * - ICME velocity

     - output

     - PNG image

     - Visualization of the distribution of the velocity of the ICME at target

     -

     -

   * - Travel time

     - output

     - PNG image

     - Visualization of the distribution of the travel time of the ICME at target

     -

     -