Hovering control for quadrotor aircraft based on finite-time control algorithm
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In this paper, a finite-time controller is proposed for the quadrotor aircraft to achieve hovering control in a finite time. The design of controller is mainly divided into two steps. Firstly, a saturated finite-time position controller is designed such that the position of quadrotor aircraft can reach any desired position in a finite time. Secondly, a finite-time attitude tracking controller is designed, which can guarantee that the attitude of quadrotor aircraft converges to the desired attitude in a finite time. By homogenous system theory and Lyapunov theory, the finite-time stability of the closed-loop systems is given through rigorous mathematical proofs. Finally, numerical simulations are given to show that the proposed algorithm has a faster convergence performance and a stronger disturbance rejection performance by comparing to the PD control algorithm.
KeywordsQuadrotor aircraft Finite-time control algorithm Hovering control
This work was supported by National Natural Science Foundation of China (61673153,61304007,) the Scientific Research and Development Funds of Hefei University of Technology (JZ2016HGXJ0023), and the Fundamental Research Funds for the Central Universities (JZ2016HGTA0700).
- 4.Hamel, T., Mahony, R., Lozano, R., Ostrowski, J.: Dynamic modelling and configuration stabilization for an X4 Flyer. IFAC Trienn. World Congr. 35(1), 217–222 (2002)Google Scholar
- 9.Khalil, H.K.: Nonlinear System, 3rd edn. Prentice hall, Upper Saddle River (2002). 303–334Google Scholar
- 12.Liu, H., Li, D.J., Zuo, Z.Y., Zhong, Y.S.: Robust three-loop trajectory tracking control for quadrotors with multiple uncertainties. IEEE Trans. Ind. Electron. 63(4), 2263–2273 (2016)Google Scholar
- 13.Yu, Y., Li, B., Hu, Q.: Quaternion-based output feedback attitude control for rigid spacecraft with bounded input constraint. In: The 34th Chinese Control Conference, pp. 489–493 (2015)Google Scholar
- 16.Bhat, S., Bernstein, D.: Finite-time stability of homogeneous systems. Am. Control Conf. 4(4), 2513–2514 (1997)Google Scholar
- 31.Hughes, P.: Spacecraft Attitude Dynamics. Wiley, Hoboken (1986)Google Scholar