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Adaptive Control with Parameters Compensator for Aircraft Boundary Control System

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Recent Developments in Mechatronics and Intelligent Robotics (ICMIR 2017)

Part of the book series: Advances in Intelligent Systems and Computing ((AISC,volume 691))

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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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Correspondence to Qian Kun .

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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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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-70989-5

  • Online ISBN: 978-3-319-70990-1

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