Quick start : Différence entre versions
(→Launch the main GUI) |
(→Initialize mandatory data) |
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Ligne 11 : | Ligne 11 : | ||
=== Initialize mandatory data === | === Initialize mandatory data === | ||
− | Then, it has been decided to avoid to get | + | Then, it has been decided to avoid to get "dangerous" default values. So, the following parameters must be initialized: |
− | * orbital parameters | + | * orbital parameters (initially set to zero) as it is not very clever to give a "default" orbit; |
− | * attitude law | + | * attitude law, even if a default law is available. Indeed, if we had decided to set by default a certain attitude law, the risk for the user was not to pay attention to it even when he will decide later to propagate, for example, with a drag force model and a non spherical shape. And it that case, the attitude law will change the final trajectory. |
==== Initial orbit ==== | ==== Initial orbit ==== | ||
Ligne 26 : | Ligne 26 : | ||
==== Dry mass ==== | ==== Dry mass ==== | ||
− | It is possible to let the | + | It is possible to let the initial dry mass to zero as below. Nevertheless, if the user will add some forces, attitudes or anything that needs to divide by the total mass, then, an error message will be sent and the propagation will not be launched. |
[[Fichier:FirstUse3.png|800px]] | [[Fichier:FirstUse3.png|800px]] |
Version du 16 novembre 2017 à 11:37
PSIMU proposes a lot of options and configurations to propagate an orbit. Anyway, in order to allow to start first simulations very quickly, the PSIMU GUI, many parameters are set to default values.
Sommaire
Launch the main GUI
To launch the GUI you only have to double click on Windows systems or type :
java -jar psimu-xx.x-jar-with-dependencies.jar
The first time, the GUI is launched a specific directory (where result files will be stored) will be created : OUTPUT_JPSIMU
Initialize mandatory data
Then, it has been decided to avoid to get "dangerous" default values. So, the following parameters must be initialized:
- orbital parameters (initially set to zero) as it is not very clever to give a "default" orbit;
- attitude law, even if a default law is available. Indeed, if we had decided to set by default a certain attitude law, the risk for the user was not to pay attention to it even when he will decide later to propagate, for example, with a drag force model and a non spherical shape. And it that case, the attitude law will change the final trajectory.
Initial orbit
Enter a non nul semi mlajor axis (for example 7000 km) in the orbit tab:
Attitude law
Select the default law as the single attitude law.
Dry mass
It is possible to let the initial dry mass to zero as below. Nevertheless, if the user will add some forces, attitudes or anything that needs to divide by the total mass, then, an error message will be sent and the propagation will not be launched.
Propagate
At the end, we have just to start the propagation by clicking on the Start button ...