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https://github.com/ME-561-W20-Quadcopter-Project/Quadcopter-Control.git
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Final Version
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@@ -56,8 +56,8 @@ z0 = 0;
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xdot0 = 0;
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xdot0 = 0;
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ydot0 = 0;
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ydot0 = 0;
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zdot0 = 0;
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zdot0 = 0;
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phi0 = 5*(pi/180)*0;
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phi0 = 10*(pi/180);
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theta0 = 5*(pi/180)*0;
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theta0 = 10*(pi/180);
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psi0 = 0;
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psi0 = 0;
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phidot0 = 0;
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phidot0 = 0;
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thetadot0 = 0;
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thetadot0 = 0;
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@@ -76,8 +76,8 @@ kdt = 0.1;
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kpps = 0.0901;
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kpps = 0.0901;
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kdps = 0.0486;
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kdps = 0.0486;
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kpz = 4.0670;
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kpz = 3.9691;
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kdz = 2.9031;
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kdz = 2.7627;
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%% Load LQR gains
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%% Load LQR gains
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LQRGoal1 = matfile('FiniteLQRGoal_1_K.mat');
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LQRGoal1 = matfile('FiniteLQRGoal_1_K.mat');
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