From 01ad37374e485282e37e3e35917d233f22e6bc53 Mon Sep 17 00:00:00 2001
From: Mauco03 <marco.gaibotti@skywarder.eu>
Date: Sun, 27 Apr 2025 00:29:28 +0200
Subject: [PATCH] [alpha-phi] Updated aerodynamic matrices

---
 .../2025_Orion_Portugal_October/data/aeroCoefficients.mat     | 4 ++--
 .../data/aeroCoefficientsHighAOA.mat                          | 4 ++--
 missions/2025_Orion_Roccaraso_September/config/rocketConfig.m | 1 +
 3 files changed, 5 insertions(+), 4 deletions(-)

diff --git a/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat b/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat
index b3c1b23..3aa85db 100644
--- a/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat
+++ b/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat
@@ -1,3 +1,3 @@
 version https://git-lfs.github.com/spec/v1
-oid sha256:75ad0a581c512de8f345a79f16d8e3d2bf681547eb386ce000434c66d6b292e0
-size 288267248
+oid sha256:f4ad48c4d016c33811361e5823e3fb0c87ae64679ff148293e2fcbb48c52f056
+size 300753532
diff --git a/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat b/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat
index 9bd98f0..00d9ce5 100644
--- a/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat
+++ b/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat
@@ -1,3 +1,3 @@
 version https://git-lfs.github.com/spec/v1
-oid sha256:da4a2977b055341314ba88e9698ffbac9702c2e57e9b876c67ea2da01631b783
-size 40438794
+oid sha256:1659d1dc6b19ea13c3cdd75b8f9627d42123c4cb6dff535d93618247a17ab9d1
+size 46224320
diff --git a/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m b/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m
index c4e1ffc..e320c15 100644
--- a/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m
@@ -19,6 +19,7 @@ rocket.lengthCenterNoMot = [];                                          % [m]
 %   When false, coefficients are saved with current motor's name
 %   When true,  coefficients are saved as 'generic'
 rocket.dynamicDerivatives = false;                                    % [-]      True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false;                                     % [-]      True if separate matrix for high AOA will be loaded
 
 %% PLD - Includes Parafoil + Nose
 parafoil = Parafoil();
-- 
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