Abstract

Introduction: We present a bio-inspired global finite time control using global fast-terminal sliding mode controller and radial basis function network to address the attitude tracking control problem of the three degree-of-freedom four rotor hover system. The proposed controller provides convergence of system states in a pre-determined finite time and estimates the unmodeled dynamics of the four rotor system. Methods: The dynamic model of the four rotor system is derived from Newton’s force equations. The unknown dynamics of the four rotor systems are estimated using Radial basis function. The bio-inspired global fast terminal sliding mode controller is proposed to provide chattering free finite time error convergence and to provide optimal tracking of the attitude angles while being subjected to unknown dynamics. The global stability proof of the designed controller is provided on the basis of the Lyapunov stability theorem. Results: The proposed controller is validated by (i) conducting an experiment through implementing it on the laboratory based hover system, and (ii) through simulations. Performance of the proposed control scheme is also compared with classical and intelligent controllers. The performance comparison exhibits that the designed controller has quick transient response and improved chattering free steady state performance. Conclusion: The proposed bio-inspired global fast terminal sliding mode controller offers improved estimation and better tracking performance than the traditional controllers. In addition, the proposed controller is computationally cost effective and can be implanted on multirotor unmanned air vehicles with limited computational processing capabilities.

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