diff --git a/aerodynamicsOptimization/README.md b/aerodynamicsOptimization/README.md
index 35c51ca1c583df34e9585f7490911173409a47e4..644dab356dd1540a46f4d832b204976bbf2054b5 100644
--- a/aerodynamicsOptimization/README.md
+++ b/aerodynamicsOptimization/README.md
@@ -3,15 +3,20 @@ This is a program developed in MATLAB which implements an aerodynamic optimizati
 The rocket is optimized to reach the highest possible apogee with the chosen set of fixed parameters using a genetic algorithm. It may take some time to run, please be patient. <br/>
 
 ## Usage
-The optimization variables are the fin chords and height, the fin shape, the ogive length and shape and the boat tail length. <br/>
-The variable's range and other features can be set in the configOptimization script and quantities are integers to run faster without a big optimization loss. <br/>
-The script requires the rocket data which is taken from the `simulationsData.m` script:
+The following table shows the available optimisation parameters
 
-``` matlab
-settings.mission = 'mission_name';
-run(strcat('../data/', settings.mission, '/simulationsData'));
-```
-and variables to describe the mission-specific parameters, defined in the `configOptimization.m`:
+|     Parameter    | Number | Notes                                             |
+|:----------------:|:------:|:------------------------------------------------:|
+| Fins chord       |  1, 2  |                         -                         |
+| Fins height      |    3   |                         -                         |
+| Fins sweep       |    4   |    Measured as distance between start of chords   |
+| Ogive length     |    5   |                         -                         |
+| Ogive shape      |  6, 7  | Valid for modified Haack: edits coefficinets p, C |
+| Boat-tail length |   8    |                         -                         |
+| Nosecone type    |    9   |                         -                         |
+
+The variable's range and other features can be set in the optimisationConfig script and quantities are integers to run faster. <br/>
+The function requires the rocket data, taken from the `rocketConfig.m` script and variables to describe the mission-specific parameters, defined in `optimisationConfig.m`:
 
 ``` matlab
 % mission information
@@ -21,18 +26,18 @@ vars.Beta = linspace(-20, 20, 20);
 vars.Alt = linspace(0, 4000, 5);
 vars.xcg = settings.xcg; 
 ```
-You have to replace `mission_name` with the specific name of the mission required. <br/>
-Moreover, the variables that cannot be known a priori, like the flight conditions, the wind magnitude or the minimum required stability margin at the launchpad exit, are taken from the `configOptimization.m` script. The variable `expectedApogee` actually allows you to set the tolerance of the genetic algorithm, so the higher is the expected apogee, the lower is the tolerance and the more precise is the optimization. <br/>
-It is also important to set the matrix of inequalities in `configOptimization.m` that acts as constraint on the optimization variables as required from the GA. <br/>
-The optimization is started by running the `mainOptimization.m` script.
+
+The variables that cannot be known a priori, like the flight conditions, the wind magnitude or the minimum required stability margin at the launchpad exit, are taken from the `optimisationConfig.m` script. The variable `expectedApogee` actually allows you to set the tolerance of the genetic algorithm, defined as $tol = \frac{1}{\texttt{Apogee}_{exp}}$ so the higher is the expected apogee, the lower is the tolerance and the more precise is the optimization. <br/>
+It is also important to set the matrix of inequalities in `optimisationConfig.m` that acts as constraint on the optimization variables as required from the GA. <br/>
+The optimization is started by running the `mainOptimization.m` function.
 
 
 ## Options
 You can optimize the rocket and the boat tail or just the rocket, keeping the boat tail fixed:<br/>
 
-* In the first case, you have to set `settings.boatOptimization = false;` in `configOptimization.m`. In this scenario, you have to also set the parameters describing the boat tail in `simulationsData`.
+* In the first case, you have to set `settings.boatOptimization = false;` in `optimisationConfig.m`. In this scenario, you have to also set the parameters describing the boat tail in `simulationsData`.
 
-* In the second case, you have to set `settings.boatOptimization = true;` in `configOptimization.m`. In this scenario, you have also to set the parameters describing the boundaries of the optimization, which are `settings.optimBoatD`, `settings.maxBoatL` and `settings.maxBeta` and check that the matrix of inequalities is suitable with the geometry of the rocket you are trying to optimize. Please note that the process will take more time.
+* In the second case, you have to set `settings.boatOptimization = true;` in `optimisationConfig.m`. In this scenario, you have also to set the parameters describing the boundaries of the optimization, which are `settings.optimBoatD`, `settings.maxBoatL` and `settings.maxBeta` and check that the matrix of inequalities is suitable with the geometry of the rocket you are trying to optimize. Please note that the process will take more time.