Abstract

Abstract. Electro-hydrostatic actuator (EHA) is an important form of power-by-wire (PBW) technology, which is widely used in aircraft because of the characteristics of small size, high power and light weight. However, the current traditional EHA with fixed pump displacement and variable motor speed (FPVM-EHA) has the problems of high energy consumption and heating of the motor under heavy load. An improved EHA with high-pressure load sensing (HPLS-EHA) is proposed in this paper, which can reduce the pump displacement under heavy load, so as to achieve reducing the torque and heating of the motor, solving the problem of high energy consumption of EHA system and improving the efficiency. The co-simulation model of the FPVM-EHA and the HPLS-EHA was established using the software programs AMESim and MATLAB, and then the simulation results are analysed. The simulation results show that the HPLS-EHA can reduce the torque and heat flow rate of the motor by 23.20 % and 41.02 % under the load of 20.2 MPa, and the fluctuation times and amplitude of output position are also reduced under varying loads at 5 s, but it will slightly reduce the position accuracy of the EHA system. In order to solve this problem, the fuzzy PID control strategy is adopted for the HPLS-EHA. The simulation results show that the position accuracy and response speed of the HPLS-EHA based on fuzzy PID are improved, the output position is improved from 8.93 to 9.25 mm, better than 9.19 mm of the FPVM-EHA, and it also maintains the advantages of low motor torque, heating and output position fluctuation.

Highlights

  • Due to the low efficiency and complex structure of the traditional aircraft control system with the central hydraulic oil source, it has become the main constraint to improve the performance of the aircraft control system (Botten et al, 2000)

  • When the load pressure is less than 10 MPa, the control mode is constant pump displacement and variable motor speed, and the plunger pump outputs the hydraulic oil according to the motor speed to drive the cylinder to work

  • The hydraulic system is established by the AMESim platform, and the control system is established by the MATLAB platform (Ji et al, 2016)

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Summary

Introduction

Due to the low efficiency and complex structure of the traditional aircraft control system with the central hydraulic oil source, it has become the main constraint to improve the performance of the aircraft control system (Botten et al, 2000). The FPVM-EHA is commonly used in aircraft, but for this kind of EHA, when the system bears a heavy load, the motor needs to output a large current to overcome the load torque, resulting in high heating and low efficiency of the system (Li et al, 2017). In response to these problems, the researchers conducted a number of studies.

Principle of displacement regulator with HPLS
Experimental verification of displacement regulator with HPLS
Composition and working principle of the HPLS-EHA
Establishment of simulation model
Simulation analysis of the HPLS-EHA
Simulation analysis of HPLS-EHA based on fuzzy PID
Design of fuzzy PID controller
Simulation analysis of the HPLS-EHA based on fuzzy PID
Findings
Conclusions
Full Text
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