diff --git a/autoMatricesProtub/autoMatProtubConfig.m b/autoMatricesProtub/autoMatProtubConfig.m
index 52ed171d4cbf7754821a7ec1e57485d0de4587c5..4cb74fbae69e4e0cbb2e4d9f63dd6792344c37a3 100644
--- a/autoMatricesProtub/autoMatProtubConfig.m
+++ b/autoMatricesProtub/autoMatProtubConfig.m
@@ -24,21 +24,17 @@ set(groot,'defaultLegendInterpreter','latex');
 
 %% STATES
 % State values in which the aerodynamic coefficients will be computed
-vars.mach = 0.05:0.05:1;
-vars.alpha = [0 0.1 0.5 1 2.5 5 7.5 10 35 60 90.1 115 130 170];
+vars.mach = 0.1:0.1:1;
+% vars.alpha = [-60 -35 -10 -7.5 -5 -2.5 -1 -0.5 -0.1 0 0.1 0.5 1 2.5 5 7.5 10 35 60];
+% vars.beta = [-10 -7.5 -5 -2.5 -1 -0.5 -0.1 0 0.1 0.5 1 2.5 5 7.5 10];
+vars.alpha = [0 0.1 0.5 1 2.5 5 7.5 10 35 60];
 vars.beta = [];
-vars.phi = 0:24:336;            % phi = 0:(360/nFins)
+% vars.phi = [];
+vars.phi = 0:24:360;            % phi = 0:(360/nFins)
 vars.alt = (0:400:4000);        % above local ground (env.z0 will be added in main)
 
 % xcg discretization
 vars.Nxcg = 3;                   % Number of wanted xcgs in order to generate N aerodynamic matrices
 
-%% HIGH AOA
-% varsHighAOA.mach = 0.05:0.05:0.7;
-% varsHighAOA.alpha = [0 1 5 10 35 60 90.1 115 130 170];
-% varsHighAOA.beta  = [];
-% varsHighAOA.phi = 0:12:120;         % phi = 0:(360/nFins)
-% varsHighAOA.alt = (0:400:4000);     % above local ground (env.z0 will be added in main)
-
 %% FINS CN partial output
 saveFinsCN = false;
\ No newline at end of file
diff --git a/autoMatricesProtub/mainAutoMatProtub.m b/autoMatricesProtub/mainAutoMatProtub.m
index 55798cc7b24578f09711f1cb9545c023319e3455..3b94be9ac0c638be51b3594082a9f225d417ae4c 100644
--- a/autoMatricesProtub/mainAutoMatProtub.m
+++ b/autoMatricesProtub/mainAutoMatProtub.m
@@ -1,4 +1,4 @@
-function [coeffsTot, coeffsTotHighAOA] = mainAutoMatProtub(rocket, environment, settings, options)
+function coeffsTot = mainAutoMatProtub(rocket, environment, settings, options)
 arguments
     rocket = []; % Empty by default
     environment Environment = Environment.empty
@@ -22,11 +22,9 @@ if isempty(settings), autoMatSettings = Settings('autoMatProtub'); end
 %% FINALIZE CONFIG (with data not directly editable)
 % correcting altitudes
 autoMatSettings.vars.alt = autoMatSettings.vars.alt + environment.z0;
-% autoMatSettings.varsHighAOA.alt = autoMatSettings.varsHighAOA.alt + environment.z0;
 
 % adding airbrakes length
 autoMatSettings.vars.hprot = rocket.airbrakes.height;
-% autoMatSettings.varsHighAOA.hprot = [];
 
 % overriding xcg number if the motor is solid
 if rocket.motor.type == MotorType.Solid && autoMatSettings.vars.Nxcg ~= 2