Abstract
This paper proposed a method of adaptive controller with a lead-lag parameters compensator and applied to a kind of aircraft boundary control system (ABCS). This method ensures optimization of fuzzy logic control function, and guarantees on-line adaptation of domain in aircraft boundary control system, which can make a great progress in dynamic characteristics and adaptabilities of flight control system. A proposed hybrid adaptation algorithm has been tested in the analogy flight practice speed control system of an induction motor drive. The digital simulation results demonstrated that it could improve transient properties in flight boundary control system, and provide well disturbance rejection in spite of its simplicity.
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References
Qian, K., Liao, K., Liu, K.: Identification of complex systems using multiple-model adaptive estimation algorithms. In: Proceedings of International Conference on EME 2015, Wuhan, China, vol. 1, pp. 870–876 (2015)
Fan, Y., Wang, W., Jiang, X.: Generalized fuzzy hyperbolic model adaptive control design for a class of nonlinear systems. Control Decis. 31(3), 417–422 (2016)
Qian, K., Xie, S., Hu, J.: Aerial pneumatic servo system based on modified feedback linearization control. Control Theory Appl. 23(3), 465–467 (2005)
Gao, X., Ren, X.: Prescribed performance adaptive control for hysteresis hammerstein system. Trans. Beijing Inst. Technol. 36(4), 412–416 (2016)
Li, D., Wu, B., Zhang, Y.: Robust adaptive control for spacecraft attitude tracking with unknown friction torque of reaction wheel. J. Astronaut. 37(2), 175–181 (2016)
Qian, K., Pang, X., Li, B.: Neural network identifier with iterative learning for turbofan engine rotor speed control system. In: Proceedings of CIS 2008, Chengdu, China, vol. 1, pp. 94–98 (2008)
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Kun, Q., Kai, L., Hao, Y., Kaijun, L. (2018). Adaptive Control with Parameters Compensator for Aircraft Boundary Control System. In: Qiao, F., Patnaik, S., Wang, J. (eds) Recent Developments in Mechatronics and Intelligent Robotics. ICMIR 2017. Advances in Intelligent Systems and Computing, vol 691. Springer, Cham. https://doi.org/10.1007/978-3-319-70990-1_62
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DOI: https://doi.org/10.1007/978-3-319-70990-1_62
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