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Robust Adaptive Attitude Stabilization of a Fighter Aircraft in the Presence of Input Constraints | ||
Journal of Electrical and Computer Engineering Innovations (JECEI) | ||
مقاله 6، دوره 4، شماره 2 - شماره پیاپی 8، مهر 2016، صفحه 149-155 اصل مقاله (1.04 M) | ||
نوع مقاله: Original Research Paper | ||
شناسه دیجیتال (DOI): 10.22061/jecei.2017.575 | ||
نویسندگان | ||
M. Bahmani؛ T. Binazadeh* | ||
Department of Electrical and Electronic Engineering, Shiraz university of Technology, Shiraz, Iran. | ||
تاریخ دریافت: 15 آبان 1395، تاریخ بازنگری: 14 دی 1395، تاریخ پذیرش: 28 دی 1395 | ||
چکیده | ||
The problem of attitude stabilization of a fighter aircraft is investigated in this paper. The practical aspects of a real physical system like existence of external disturbance with unknown upper bound and actuator saturation are considered in the process of controller design of this aircraft. In order to design a robust autopilot in the presence of the actuator saturation, the Composite Nonlinear Feedback (CNF) controller along with the Adaptive Integral Sliding Mode (AISM) controllerand the new robust controller that is called AISM-CNF control law is proposed. The CNF part of controller is used for stabilization of the nominal system and also improvement of the transient performance by considering the actuator saturation. The AISM part guarantees robustness against the model uncertainties and/or external disturbances. Since in the proposed approach, the upper bound of the uncertain terms is estimated and therefore there is no need to the prior knowledge of the upper bound of the model uncertainties. Finally, simulation results show the performance of the proposed AISM-CNF controller in term of attitude stabilization of fighter aircraft, robustness, and the good characteristics of the transient responses of the autopilot system in spite of actuator saturation and external disturbance. | ||
کلیدواژهها | ||
Fighter Aircraft؛ Input Constraints؛ Composite Nonlinear Feedback (CNF)؛ Adaptive Integral Sliding Mode (AISM) | ||
مراجع | ||
[1] T. Yamasaki, S.N. Balakrishnan, and H. Takano, “Integrated guidance and autopilot design for a chasing UAV via highorder sliding modes,” Journal of the Franklin Institute, vol. 349, no. 2, pp. 531–558, 2012.
[2] B. Chen, Z. Jiao, and Sh.S. Ge, “Aircraft-on-ground path following control by dynamical adaptive backstepping,” Chinese Journal of Aeronautics, vol. 26, no. 3, pp. 668–675, 2013.
[3] J.W. Wang, H.N. Wu, L. Guo, and Y.S. Luo, “Robust H∞ fuzzy control for uncertain nonlinear Markovian jump systems with time-varying delay,” Fuzzy Sets and Systems, vol. 212, no. 1, pp. 41–61, 2013.
[4] K. Peng, G. Cai , B.M. Chen, M. Dong, K.Y. Lum, and T.H. Lee, “Design and implementation of an autonomous flight control law for a UAV helicopter,” Automatica, vol. 45, no. 10, pp. 2333–2338, 2009.
[5] W. Lan, B.M. Chen, and Y. He, “On improvement of transient performance in tracking control for a class of nonlinear systems with input saturation,” Systems & Control Letters, vol. 55, no. 2, pp. 132–138, 2006.
[6] Z. Zhu, Y. Xia, and M. Fu, “Adaptive sliding mode control for attitude stabilization with actuator saturation,” IEEE Transactions on Industrial Electronics, vol. 58, no. 10, pp. 4898- 4907, 2011.
[7] K. Lu, Y. Xia, and M. Fu, “Controller design for rigid spacecraft attitude tracking with actuator saturation,” Information Sciences, vol. 220, no. 2, pp. 343–366, 2013.
[8] A.R. Teel, “Anti-windup for exponentially unstable linear systems,” International Journal of Robust Nonlinear Control, vol. 9, no. 10, pp. 701–716, 1999.
[9] M.L. Workman, “Adaptive proximate time optimal servomechanisms,” Ph.D. dissertation, Stanford University, Stanford, CA, 1987.
[10] B.M. Chen, T.H. Lee, K. Peng, and V. Venkataramanan, “Composite nonlinear feedback control for linear systems with input saturation: theory and an application,” IEEE Transactions on Automatic Control, vol. 48, no. 3, pp. 427–439, 2003. [11] Y. He, B.M. Chen, and C. Wu, “Composite nonlinear control with state and measurement feedback for general multivariable systems with input saturation,” Systems Control Letters, vol. 54, no. 5, pp. 455–469, 2005.
[12] T. Binazadeh and M. Bahmani, “Robust time-varying output tracking control in the presence of actuator saturation,” Transactions of the Institute of Measurement and Control (2016), DOI: https://doi.org/10.1177/0142331216650022
[13] J. Wang and J. Zhao, “On improving transient performance in tracking control for switched systems with input saturation via composite nonlinear feedback,” International Journal of Robust and Nonlinear Control, vol. 26, no. 9, pp. 509-518, 2015.
[14] L. Wei, F. Fang, and Y. Shi, “Adaptive backstepping-based composite nonlinear feedback water level control for the nuclear utube steam generator,” IEEE Transactions on Control Systems Technology, vol. 22, pp. 369-377, 2014.
[15] W. Lan, C. K. Thum, and B. M. Chen, “A hard-disk-drive servo system design using composite nonlinear-feedback control with optimal nonlinear gain tuning methods,” IEEE Transactions on Industrial Electronics, vol. 57, pp. 1735-1745, 2010.
[16] G. Cheng and K. Peng, “Robust composite nonlinear feedback control with application to a servo positioning system,” IEEE Transactions on Industrial Electronics, vol. 54, pp. 1132-1140, 2007.
[17] B. Bandyopadhyay, F. Deepak, and K.-S. Kim, “Integral sliding mode based composite nonlinear feedback control,” in Sliding Mode Control Using Novel Sliding Surfaces, ed: Springer, pp. 83-95, 2009.
[18] Z. Zheng, W. Sun, H. Chen, and J. T. Yeow, “Integral sliding mode based optimal composite nonlinear feedback control for a class of systems,” Control Theory and Technology, vol. 12, pp. 139-146, 2014.
[19] A. Isidori, Nonlinear Control Systems, Springer, London, 1995
[20] http://www.klabs.org/DEI/References/contents_detailed/air craft_nomenclature/index.htm.
[21] H.K. Khalil, Nonlinear systems, 3rd edition, Prentice hall, 2002.
[22] H.J. Sussmann, P.V. Kokotovic, “The peaking phenomenon and the global stabilization of nonlinear systems,” IEEE Transactions on Automatic Control, vol. 36, no. 4, pp. 424–440, 1991.
[23] W. Lan and B.M. Chen, “On selection of nonlinear gain in composite nonlinear feedback control for a class of linear systems,” in Proc. 46th IEEE Conference on Decision and Control Conf., New Orleans, LA, USA, pp. 12-14.
[24] F. Castanos and L. Fridman, “Analysis and design of integral sliding manifolds for systemswith unmatched perturbations,” IEEE Transactions on Automatic Control, vol. 51, no. 5, pp. 853– 858, 2006.
[25] V.I., Utkin and J. Shi, “Integral sliding mode in systems operating under uncertainty conditions,” in Proc. 35th conference on decision and and control, Conf., Kobe, Japan, pp. 4591–4596, 1996.
[26] F.J. Bejarano, L. Fridman, and A. Poznyak, “Output integral sliding mode control based on algebraic hierarchical observer,” International Journal of Control, vol. 80, no. 3, pp. 443–453, 2006.
[27] V.I. Utkin, “Variable structure system with sliding mode,” IEEE Transactions on Automatic Control, vol. 22, no. 2, pp. 212–221, 1977.
[28] V.I. Utkin, J. Guldner, and J. Shi, Sliding Mode Control in Electromechanical Systems, Taylor & Francis, Abington, 1999.
[29] J. E. Slotine and W. Li, Applied Nonlinear Control, Englewood Cliffs, NJ: Prentice-Hall, 1991. | ||
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