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https://github.com/ME-561-W20-Quadcopter-Project/Quadcopter-Control.git
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Merge branch 'master' into nonlinear
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@@ -56,14 +56,15 @@ z0 = 0;
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xdot0 = 0;
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ydot0 = 0;
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zdot0 = 0;
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phi0 = 10*(pi/180);
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theta0 = 10*(pi/180);
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phi0 = 5*(pi/180)*0;
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theta0 = 5*(pi/180)*0;
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psi0 = 0;
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phidot0 = 0;
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thetadot0 = 0;
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psidot0 = 0;
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initialCondition = [x0, y0, z0, xdot0, ydot0, zdot0, phi0, theta0, psi0, phidot0, thetadot0, psidot0];
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%%
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%Gains
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kpp = 0.4754;
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@@ -80,4 +81,5 @@ kdz = 2.9031;
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Q = zeros(12); Q(7:9, 7:9) = eye(3);
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R = 1;
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%K = lqr(A,B,Q,R);
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%K = lqr(A,B,Q,R);
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