Skip to content
GitLab
Explore
Sign in
caesar
WP2330
wiki
Compare revisions
a8fb0c6d25a20f5dfdf7b9aab83b8f35baa6fd34 to 9a5db78e19779ca3046714e513fb4eb3b84d39ed
Commits on Source (2)
pdbmodel added
· 290e8744
Stefano Scardigli
authored
Apr 17, 2024
290e8744
Merge branch 's3_dev' into 'main'
· 9a5db78e
Valerio Formato
authored
Apr 17, 2024
pdbmodel added See merge request
!19
9a5db78e
Hide whitespace changes
Inline
Side-by-side
docs/source/products/software/unitov_pdb_model.rst
0 → 100644
View file @
9a5db78e
==================================
UNITOV P-DBM CME propagation model
==================================
.. 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
-
-