Systems Engineering and Electronics ›› 2018, Vol. 40 ›› Issue (2): 393-400.doi: 10.3969/j.issn.1001-506X.2018.02.22

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Aircraft anti-windup of robust adaptive nonlinear predictive control

WANG Chao1, ZHANG Shengxiu2, SONG Zibiao1, YANG Jianye1, WU Xiaolu1   

  1. 1. Sergeancy Academy, Rocket Force University of Engineering , Qingzhou 262500, China; 2. Department ofAutomatic Control Engineering, Rocket Force University of Engineering, Xi’an 710025, China
  • Online:2018-01-25 Published:2018-01-23

Abstract: Aiming at the performance of the adaptive nonlinear model predictive flight controller degraded greatly when big external disturbance and model parameter uncertainties exist simultaneously, a robust adaptive nonlinear predictive controller with fuzzy disturbance observer compensation-robust adaptive nonlinear model predictive control (FDO-RANMPC) is proposed. Firstly, a recursive least squares method with restrictions on unknown parameters is employed for online identification of model parameters; Secondly, by using FDO output value to compensate and eliminate the larger composite disturbance, and by using Tube RMPC control strategy, a FDO-RANMPC flight controller with guaranteed stability is developed; Finally, simulation results for attitude command tracking in the presence of composite disturbance demonstrate the applicability and the asymptotic stability of the designed controller.

CLC Number: 

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