| Citation: | XIE M J，DUAN J Q，MA W R，et al. Sliding mode control for electric braking systems of aircraft based on prescribed performance[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：260-267 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0229
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The aircraft’s electric antiskid braking system has strong nonlinear characteristics, and the interference in the electromechanical actuator (EMA) is not conducive to system stability, a sliding mode backstepping control method based on finite-time prescribed performance control is proposed. An electric antiskid braking system model with slip rate subsystem and EMA subsystem is established based on reasonable simplification with the finite time convergence prescribed performance function introduced. Based on the backstepping design, a finite-time prescribed performance control algorithm is designed to generate reference braking pressure for the slip rate controller, which can limit the slip tracking error in the predefined bounds within a finite time by appropriately choosing design parameters. Using a control algorithm for the nonsingular terminal sliding mode, the EMA controller is designed. To improve EMA subsystem robustness and precision, an extended state observer is designed, which can estimate and compensate the disturbances. Simulation results verity the control effects of the proposed method for dry and ice runways.
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