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Title: Attitude observer-based robust control for a twin rotor system (English)
Author: Salas, Oscar
Author: Castañeda, Herman
Author: De León-Morales, Jesús
Language: English
Journal: Kybernetika
ISSN: 0023-5954
Volume: 49
Issue: 5
Year: 2013
Pages: 809-828
Summary lang: English
Category: math
Summary: In this paper, an angular tracking control based on adaptive super twisting algorithm (ASTA) for a Twin Rotor System is presented. With the aim of implementing the ASTA control and taking into consideration the difficulties of measuring some of its states, a Nonlinear Extended State Observer (NESO) is employed to estimate the vector state and furthermore unmeasured dynamics. This scheme increases robustness against unmodeled dynamics and external disturbance, reducing modeling difficulties due to the fact that it is not necessary to know all the parameters of the system. Furthermore, an analysis of stability is provided, where sufficient conditions are given in order to guarantee the stability of the closed-loop system. Experimental results demonstrate the feasibility of the control scheme and illustrate its performance under external disturbance. (English)
Keyword: robust adaptive control
Keyword: extended state observer
Keyword: flight control
MSC: 62A10
MSC: 93C40
MSC: 93E12
idZBL: Zbl 1278.93283
idMR: MR3182642
Date available: 2013-11-27T10:00:30Z
Last updated: 2015-03-29
Stable URL:
Reference: [1] Anon1: Two Rotor Aero-dynamical System. User's manual..Inteco Ltd., 2006.
Reference: [2] Ahmed, Q., Bhatti, A., Iqbal, S., Kazmi, I.: 2-sliding mode based robust control for 2-dof helicopter..In: 11th Internat. Workshop on Variable Structure Systems 2010, pp. 481-486.
Reference: [3] Azam, M., Singh, S. N.: Invertibility and trajectory control for nonlinear maneuvers of aircraft..J. Guidance, Control and Dynamics 17 (1998), 1, 192-200. Zbl 0800.93406, 10.2514/3.21178
Reference: [4] Dutka, A., Ordys, A., Grimble, M.: Non-linear predictive control of 2 dof helicopter model..In: Proc. 42nd IEEE Conference on Decision and Control 2003.
Reference: [5] Freidovich, L. B., Khalil, H. K.: Performance recovery of feedback-linearization-based designs..IEEE Trans. Automat. Control 53 (2008), 10, 2324-2334. MR 2466587, 10.1109/TAC.2008.2006821
Reference: [6] Filippov, A.: Differential Equation with Discontinuos Right-Hand Side..Kluwer 1988.
Reference: [7] Gao, Z.: Scaling and bandwidth - parametrization based controller tuning..In: IEEE Proc. American Control Conference, Denver 2003, pp. 4989-4996.
Reference: [8] Guo, B. Z., Zhao, Z. L.: On convergence of non-linear extended state observer for multi-input multi-output systems with uncertainty..IET Control Theory Appl. 6 (2012), 15, 2375-2386. MR 3057797, 10.1049/iet-cta.2012.0123
Reference: [9] Khalil, H. K.: Nonlinear Systems..Prentice Hall, Englewood Cliffs, NJ 2002. Zbl 1194.93083
Reference: [10] Kokotovic, P. V., Khalil, H. K.: Singular Perturbation Methods in Control: Analysis and Design..Academic Press, London 1986. Zbl 0989.93001, MR 0937051
Reference: [11] Levant, A.: High-order sliding modes, differentiation and output-feedback control..Internat. J. Control 76 (2003), 9-10, 924-941. MR 1999375, 10.1080/0020717031000099029
Reference: [12] Lopez-Martinez, M., Rubio, F.: Approximate feedback linearization of a laboratory helicopter..In: Proc. 6th Portuguese Conference on Automatic Control 2004, pp. 43-48.
Reference: [13] Lopez-Martinez, M., Ortega, M., Vivas, C., Rubio, F.: Nonlinear $L_2$ control of a laboratory helicopter with variable speed rotors..Automatica 43 (2007), 4, 655-661. Zbl 1114.93024, MR 2306709, 10.1016/j.automatica.2006.10.013
Reference: [14] Moreno, J., Osorio, M.: Strict Lyapunov functions for the super-twisting algorithm..IEEE Trans. Automat. Control 57 (2012), 4, 1035-1040. MR 2952337, 10.1109/TAC.2012.2186179
Reference: [15] Mullhaupt, Ph., Srinivasan, B., Levine, J., Bonvin, D.: A Toy more difficult to control than the real thing..In: Proc. European Control Conference 1999, pp. 253-258.
Reference: [16] Petkov, P., Christov, N., Konstatinov, M.: Robust real-time control of a two-rotor aerodynamic system..In: Proc. 17th IFAC World Congress 2008, pp. 6422-6427.
Reference: [17] Plestan, F., Chriette, A.: A robust controller based on adaptive super-twisting algorithm for a 3DOF helicopter..In: Decision and Control Conference 2012, pp. 7095-7100.
Reference: [18] Poznyak, A. S.: Advanced Mathematical Tools for Automatic Control Engineers..Elsevier, Deterministic Techniques 1, Amsterdam 2008, p. 774. MR 2374025
Reference: [19] Rahideh, A., Shaheed, M., Huijberts, H.: Dynamic modelling of a TRMS using analytical and empirical approaches..Control Engrg. Practice 16 (2008), 241-259. 10.1016/j.conengprac.2007.04.008
Reference: [20] Reale, G., Ortner, P., Re, L. Del: Nonlinear observers for closed-loop control of a combustion engine test bench..In: Proc. 2009 American Control Conference 6, Missouri 2009, pp. 4648-4653.
Reference: [21] Saksena, V., O'Reily, J., Kokotovic, P.: Singular perturbations and time-scale methods in control theory: Survey 1976 - 1983..Automatica 20 (1984), 273-293. MR 0748193, 10.1016/0005-1098(84)90044-X
Reference: [22] Shtessel, Y., Taleb, M., Plestan, F.: A novel adaptive-gain supertwisting sliding mode controller: methodology and application..Automatica 48 (2012), 5, 759-769. Zbl 1246.93028, MR 2912798, 10.1016/j.automatica.2012.02.024
Reference: [23] Yang, X., Huang, Y.: Capabilities of extended state observer for estimating uncertainties..In: Proc. American Control Conference 1, Missouri 2009, pp. 3700-3705.
Reference: [24] Zhu, B., Huo, W.: Trajectory linearization control for a quadrotor helicopter..In: 8th International Conference on Control and Automation 2010, pp. 34-39.


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