From 3b109f3b54d5c081bcf25a8ac9a38f11954de5d3 Mon Sep 17 00:00:00 2001
From: Mauco03 <marco.gaibotti@skywarder.eu>
Date: Thu, 12 Dec 2024 22:26:07 +0100
Subject: [PATCH] [coefficients] Removed highAoA references from
autoMatricesProtub
---
autoMatricesProtub/autoMatProtubConfig.m | 16 ++++++----------
autoMatricesProtub/mainAutoMatProtub.m | 4 +---
2 files changed, 7 insertions(+), 13 deletions(-)
diff --git a/autoMatricesProtub/autoMatProtubConfig.m b/autoMatricesProtub/autoMatProtubConfig.m
index 52ed171d..4cb74fba 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 55798cc7..3b94be9a 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
--
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