diff --git a/missions/2024_Lyra_Roccaraso_September/config/controlConfig.m b/missions/2024_Lyra_Roccaraso_September/config/controlConfig.m
index 6811037a22449eab83a437a29e1d95ebaa7ee7f1..0fe845b95d89b806324d8407f15dd8875bdead0c 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/controlConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/controlConfig.m
@@ -14,6 +14,7 @@
 %       - settings.dtControl: define the usage time of the i-th
 %                             configuration. Its length must be -1 the
 %                             length of settings.control
+control = Control();
 
 control.multipleAB = false;                                                % If true, multiple and smooth airbrakes opening will be simulated
 control.opening = [1 3];                                                   % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
diff --git a/missions/2024_Lyra_Roccaraso_September/config/conversionsConfig.m b/missions/2024_Lyra_Roccaraso_September/config/conversionsConfig.m
new file mode 100644
index 0000000000000000000000000000000000000000..3d56f8776f812cf9c00403f7dc4d8aca48ab92a0
--- /dev/null
+++ b/missions/2024_Lyra_Roccaraso_September/config/conversionsConfig.m
@@ -0,0 +1,39 @@
+% CONFIG - This script sets up control parameters
+
+settings = loadConfig("settingsConfig.m");
+geometry = loadConfig("geometryConfig.m");
+engine = loadConfig("engineConfig.m");
+
+if settings.addMfusMot
+    corrections.xcgNoMot = (geometry.mNoMot*geometry.xcgNoMot + ... 
+        engine.fuselage.mFuselage*(engine.fuselage.xcgFuselage + geometry.center.length ))...
+                        /(goemetry.mNoMot + engine.fuselage.mFuselage);
+    corrections.mNoMot = geometry.mNoMot + engine.fuselage.mFuselage;
+else
+    corrections.mNoMot = geometry.mNoMot;
+    corrections.xcgNoMot = geometry.xcgNoMot;
+end
+
+%% SYNTHESIS
+corrections.Lcenter = geometry.center.length  + engine.motor.L; % [m] Total centerbody length
+corrections.noseconeMass = 0;                                             % [kg] Nosecone Mass
+corrections.totStrMass = corrections.mNoMot + engine.motor.strMass + ...
+corrections.noseconeMass;                                                 % [kg] Total structural Mass
+corrections.m0 = corrections.totStrMass + engine.motor.expM(1);           % [kg] Total initial Mass
+corrections.mTotalTime = corrections.mNoMot + engine.motor.strMass + ...
+corrections.noseconeMass + engine.motor.expM;                           % Total mass (in time)
+
+% Total XCG of the rocket [m] !! FROM NOSECONE BASE !!
+corrections.xcg = ( (engine.motor.expM + engine.motor.strMass).*(geometry.center.length + engine.motor.xcg) + ...
+    corrections.mNoMot*corrections.xcgNoMot)./(engine.motor.expM + engine.motor.strMass + corrections.mNoMot);
+
+corrections.Lcenter = corrections.Lcenter - geometry.boat.length;         % correcting the rocket length in order to account the boat tail
+
+%% APPLY CORRECTIONS
+
+if exist("correction.mat","file")
+    correctionData = load("correction.mat");
+    corrections.mTotalTime = corrections.mTotalTime + correctionData.deltaM;
+    corrections.xcg = corrections.xcg + reshapeVector(engine.motor.expTime, correctionData.time, correctionData.deltaXcg);
+    corrections.totStrMass = corrections.totStrMass + correctionData.deltaM;
+end
\ No newline at end of file
diff --git a/missions/2024_Lyra_Roccaraso_September/config/environmentConfig.m b/missions/2024_Lyra_Roccaraso_September/config/environmentConfig.m
index 1f90f25bdb1ff9f1093f834625cccd88d6c700d4..91165eb0c3e129404492fcd01d841fb05ba05565 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/environmentConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/environmentConfig.m
@@ -2,10 +2,11 @@
 %
 % Use this file to write launch data, independent from the rocket itself
 
+environment = Environment();
+
 environment.lat0 = 41.8084579;                                   % [deg] Launchpad latitude
 environment.lon0 = 14.0546408;                                   % [deg] Launchpad longitude
 environment.z0 = 1414;                                           % [m] Launchpad Altitude
-environment.g0 = gravitywgs84(environment.z0, environment.lat0);           % Gravity costant at launch latitude and altitude
 environment.pin1Length = 000;                                      % [m] Distance from the upper pin to the upper tank cap
 environment.pin2Length = 000;                                      % [m] Distance from the lower pin to the lower tank cap  
 environment.rampLength = 000;                                         % [m] Total launchpad length 
diff --git a/missions/classes/Control.m b/missions/classes/Control.m
new file mode 100644
index 0000000000000000000000000000000000000000..1a550e55565360190d3a0ca7f123bb6c47b0946d
--- /dev/null
+++ b/missions/classes/Control.m
@@ -0,0 +1,33 @@
+classdef Control < Config
+    % CONTROL Summary of this class goes here
+    %   Detailed explanation goes here
+
+    properties
+        multipleAB      logical     % If true, multiple and smooth airbrakes opening will be simulated
+        opening         double      % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
+        deltaTime       double      % aerobrakes, configurations usage time
+        minTime         double      % [s] time after which the airbrakes can be used
+        maxMach         double      % [-] Maximum Mach at which airbrakes can be used
+        servoOmega      double      % [rad/s] Servo-motor angular velocity
+        height          double      % [m] Block airbrakes opening coordinate ( First entry must be 0! )
+    end
+
+    properties(Access = protected)
+        configName = 'controlConfig.m'
+        mission Mission
+        motor Motor
+    end
+
+    methods
+        function obj = Control(mission, motor)
+            arguments
+                mission Mission = Mission()
+                motor Motor = Motor()
+            end
+            obj.mission = mission;
+            obj.motor = motor;
+            if nargin == 0, return; end
+            obj.loadConfig();
+        end
+    end
+end
diff --git a/missions/classes/Environment.m b/missions/classes/Environment.m
index cd0f2f2e180a71ee4ad85aea98abd770e88a2b4e..6c503a6bd82519a49c3538e989c402d546b6bfdf 100644
--- a/missions/classes/Environment.m
+++ b/missions/classes/Environment.m
@@ -30,7 +30,7 @@ classdef Environment < Config
         function obj = Environment(mission, motor)
             arguments
                 mission Mission = Mission()
-                motor Motor = Mission()
+                motor Motor = Motor()
             end
             obj.mission = mission;
             obj.motor = motor;