Abstract

The electro-hydrostatic actuator (EHA), the actuator of electric drive and hydraulic transmission, is competitive since it is small in size, light in weight and high in power density. However, the existence of the velocity loop error of servo motors, unmodeled dynamics and highly nonlinear uncertainties restrict the improvement of the tracking accuracy of the EHA system. In order to achieve high-precision motion control of EHAs, a RISE-based composite adaptive control scheme is proposed in this paper. In the proposed composite adaptive control design, a novel parameter adaptive law is synthesized to compensate for the parametric uncertainties and a robust integral of the sign of error (RISE) feedback is utilized to suppress the adverse effects caused by the lumped disturbances, including the velocity loop error of a servo motor and other unmodeled dynamics. The synthesized parameter adaptive law possesses the advantage of fast convergence, which is beneficial to achieve transient tracking performance improvement. In addition, the proposed controller is more suitable for practical applications since it is chattering free. The closed-loop system stability analysis shows that the proposed control scheme guarantees an excellent asymptotic tracking performance. Finally, comparative simulations are conducted to verify the high-performance nature of the proposed controller.

Highlights

  • The hydraulic actuator servo control system is one of the key factors for flight control systems to realize the flight attitude of aircraft

  • The simulated electro-hydrostatic actuator (EHA) system relies on a servo motor to drive the plunger pump

  • (1) CARISE: The robust integral of the sign of error (RISE)-based composite adaptive controller is proposed in this paper and described in Section 3, whose control parameters are given by k1 = 400, k2= 1000, k3= 2, kr= 8, Γ = diag{5, 1000, 0.01}, k = 0.01, j = 1, β = 1 and θ(0) = [18000; 4 × 105; 10]

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Summary

Introduction

The hydraulic actuator servo control system is one of the key factors for flight control systems to realize the flight attitude of aircraft. In the airborne actuation system of aircraft, the traditional hydraulic system will gradually be replaced by the power-by-wire (PBW) flight control system due to easy leakage, low efficiency and complex pipelines. The PBW achieves the power transmission between the aircraft’s secondary energy system and the various actuators in the form of electric energy through cables, eliminating the need for a central hydraulic system and hydraulic pipelines all over the fuselage. It greatly improves the reliability, efficiency and survivability of the aircraft and contributes to the realization of multi-electric/all-electric aircraft. In the field of vibration damping and industrial actuators, the application of EHAs was realized [10,11]

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