The ***MSA toolkit*** is the repository in which the code implemented by the Mission Analysis team is stored. It is composed of several folders.
The ***MSA toolkit*** is the repository in which the code implemented by the Mission Analysis team is stored. It is composed of several folders.
In order to properly run the msa toolkit code in MATLAB, you will need to install the following MATLAB add-ons:
In order to properly run the msa toolkit code in MATLAB, you will need to install the following MATLAB add-ons:
* Aerospace Toolbox
* Global Optimization Toolbox
* Mapping Toolbox
* Optimization Toolbox
* Parallel Computing Toolbox
* Statistics and Machine Learning Toolbox
The repository itself contains the necessary tools, while the majority of the data is stored in the common folder, which is a submodule linked to the common repository
***Simulink**
***Aerospace Blockset**
***Aerospace Toolbox**
***Deep Learning Toolbox**
***Global Optimization Toolbox**
***Mapping Toolbox**
***Navigation Toolbox**
***Optimization Toolbox**
***Parallel Computing Toolbox**
***Statistics and Machine Learning Toolbox**
***Symbolic Math Toolbox**
The repository itself contains the necessary tools, while the majority of the data is stored in the common folder, which is a *submodule* linked to the common repository.
### aerodynamicsOptimization
### aerodynamicsOptimization
This program implements an aerodynamics optimization of the rocket. The rocket is optimized to reach the highest apogee possible with the chosen set of fixed parameters using a genetic algorithm. It may take some time to run.
This program implements an aerodynamics optimization of the rocket. The rocket is optimized to reach the highest apogee possible with the chosen set of fixed parameters using a genetic algorithm. It may take some time to run.
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@@ -30,7 +36,7 @@ This program is developed for a primary apogee analysis with different engines w
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@@ -30,7 +36,7 @@ This program is developed for a primary apogee analysis with different engines w
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### autoMatricesProtub
### autoMatricesProtub
This program allows for an automatic computation of the rocket aerodynamic coefficients using Missile DATCOM, for different airbrakes configurations.
This program allows for an automatic computation of the rocket aerodynamic coefficients, for different airbrakes configurations.