Backstepping sliding mode-based anti-skid braking control for a civil aircraft
Tóm tắt
Taking off and landing are critical phases and it is easy to happen flight disaster for them due to complex environment and weather. To improve flight safety of the aircraft, an anti-skid control method is proposed. First, the ground dynamics model of the civil aircraft is established. Second, a baseline controller is designed to control the velocity and yaw angle of the civil aircraft by Proportional-Integral (PI) technique. Meanwhile, considering high-speed factor during the braking phase, the braking force of the aircraft is over large, and the wheels are easy to skid. To overcome this, an anti-skid system is built, and the dynamic model of the aircraft anti-skid braking system is established. A backstepping sliding mode control algorithm is proposed to control the braking speed. And the slip ratio of the aircraft wheel is controlled by adjusting braking coefficient
$${\mu }_{Brake}$$
and the optimal slip ratio is achieved. Stability of the closed-loop system is proved by Lyapunov stability theory. Simulation results show that the proposed controller can track the desired trajectory well and the braking efficiency is optimal, which effectively shortens the braking distance of the aircraft, reduces wear of tire, and prevents puncture caused by wheel slip.
Tài liệu tham khảo
Dai Y, Yu L, Song J et al (2020) Aircraft ground braking assistant control based on pilot control model. IEEE Access 8:88643–88650
Han W, Xiong L, Yu Z (2019) Braking pressure control in electro-hydraulic brake system based on pressure estimation with nonlinearities and uncertainties. Mech Syst Signal Process 131:703–727
Jeon J W, Woo G A, Lee KC et al (2003) Developments of ABS controller for aircraft with real-time HILS system. In: Sixth International Conference on Electrical Machines and Systems, ICEMS 2003. IEEE, 2003; 2: 498–501
Coetzee EB, Krauskopf B, Lowenberg M (2006) Nonlinear aircraft ground dynamics. University of Bristol
Bo L, Zongxia J, Shaoping W (2006) Research on modeling and simulation of aircraft taxiing rectification. In: 2006 IEEE Conference on Robotics, Automation and Mechatronics. IEEE, 2006; 1–5
Zhang H, Bai N, Shang Y (2020) Modeling and simulation of aircraft ground taxiing based on flightgear visualization. In: CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020). IET, 2020, 336–340
Lan CE, Chang RC (2018) Unsteady aerodynamic effects in landing operation of transport aircraft and controllability with fuzzy-logic dynamic inversion. Aerosp Sci Technol 78:354–363
Chen B, Jiao Z, Ge SS (2013) Aircraft-on-ground path following control by dynamical adaptive backstepping. Chin J Aeronaut 26(3):668–675
Roos C, Biannic JM, Tarbouriech S et al (2010) On-ground aircraft control design using a parameter-varying anti-windup approach. Aerosp Sci Technol 14(7):459–471
Liu SQ, Sang YJ, Whidborne JF (2020) Adaptive sliding-mode-backstepping trajectory tracking control of underactuated airships. Aerosp Sci Technol 97:105610
Unsal C, Kachroo P (1999) Sliding mode measurement feedback control for antilock braking systems. IEEE Trans Control Syst Technol 7(2):271–281
Pacejka H (2005) Tire and vehicle dynamics. Elsevier, Amsterdam
Jiao Z, Wang Z, Sun D et al (2021) A novel aircraft anti-skid brake control method based on runway maximum friction tracking algorithm. Aerosp Sci Technol 110:106482
Liu Z, Su J, Li Z et al (2018) Research of reconstruction technology in aircraft anti-skid braking system based on shortest path method. CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018). IET, 645–649
Turbuk MC (2009) Taxiing maneuvers dynamics and control. Instituto Tecnológico de Aeronáutica
Jiao Z, Liu X, Li F et al (2017) Aircraft antiskid braking control method based on tire–runway friction model. J Aircr 54(1):75–84