Artificial intelligence based control of 3D inverted pendulum

In this paper the design and development of a control system for three dimensional inverted pendulum is proposed. The 3D inverted pendulum is related to rocket or missile guidance, where the center of gravity is located behind the center of drag causing aerodynamic instability. Three dimensional inverted pendulum is highly non-linear system. The Simulink model of 3D pendulum in this work is associated with the virtual world. Analysis is done on three dimensional inverted pendulum with additional position and angle into a two dimensional inverted pendulum. Comparative study of simulation results of walking control using PID controller and fuzzy logic controller are presented.