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# Nonlinear-Dynamic-Inversion-algorithm-for-quadcopter
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# Controller-algorithm-for-quadcopter
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This section has PID controller, Nonlinear dynamic inversion controller based on euler angles and body rates are provided.
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Refer : Chapter3_NDI_quad.pdf for derivation
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Also refer : https://github.com/Prabhu-369/Quadcopter_6DOF_Matlab_files.git for 6dof dervation
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Usage: call main function in matlab and the simulation would run.
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The code is modularised, if needed anyone can make use of individual functions

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