Fixed-time controller for altitude/yaw control of mini-drone based on nonsingular terminal sliding mode: Real-time implementation with uncertainties

To obtain fixed-time stability and finite-time convergence of altitude and yaw motions of a mini-quadrotor subjected to perturbations, this paper proposes a new altitude/yaw motion finite-time tracking control. First, a nonsingular terminal sliding manifold is proposed for both subsystems whose states converge to their desired values in finite-time. To address the uncertainties of the system, a robust fixed-time switching controller is proposed whose stability is proposed and its settling-time depends only on control of the parameters and not the initial conditions. The validation of the proposed approach is presented based on a real mini-quadrotor.