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implemented improved thrust curve
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@@ -59,18 +59,26 @@ figure(2)
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% Euler Angles
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subplot(2, 1, 1)
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plot(t, yaw, pitch, roll)
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hold on;
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plot(t, yaw)
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plot(t, pitch)
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plot(t, roll)
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title('Euler Angles vs Time')
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xlabel('Time (ms)')
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ylabel('Euler Angles (deg)')
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legend("yaw", "pitch", "roll")
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% Angular Velocity
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subplot(2, 1, 2)
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plot(t, yawdot, pitchdot, rolldot)
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hold on;
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plot(t, yawdot)
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plot(t, pitchdot)
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plot(t, rolldot)
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title('Angular Velocity vs Time')
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xlabel('Time (ms)')
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ylabel('Angular Velocity (deg/s)')
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saveas(gcf,'outputs/Euler Angles vs Time.png')
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legend("yawdot", "pitchdot", "rolldot")
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figure(3)
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