Performance analysis of an electro-hydrostatic actuator with high-pressure load sensing based on fuzzy PID
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Published:2021-05-18
Issue:1
Volume:12
Page:529-537
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ISSN:2191-916X
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Container-title:Mechanical Sciences
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language:en
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Short-container-title:Mech. Sci.
Author:
Zhang Hong,Ding Lan,Zhang Wentao,Li Chenchen
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.
Funder
Dalian University of Technology
Publisher
Copernicus GmbH
Subject
Industrial and Manufacturing Engineering,Fluid Flow and Transfer Processes,Mechanical Engineering,Mechanics of Materials,Civil and Structural Engineering,Control and Systems Engineering
Reference16 articles.
1. Botten, S. L., Whitley, C. R., and King, A. D.: Flight control actuation technology for next-generation all-electric aircraft, Technology Review Journal, 8, 55–68, 2000. 2. Chao, Q., Zhang, J., Xu, B., Shang, Y., Jiao, Z., and Li, Z.: Load-Sensing Pump Design to Reduce Heat Generation of Electro-Hydrostatic Actuator Systems, Energies, 11, 2266, https://doi.org/10.3390/en11092266, 2018. 3. Fu, Y.-L., Shao, Y.-B., and Qi, H.: Integrated Electro-hydrostatic Actuator System: Theory and Technology, Chinese Hydraulics and Pneumatics, 0, 1–8, https://doi.org/10.11832/j.issn.1000-4858.2015.05.001, 2015. 4. Gao, B., Fu, Y.-L., Pei, Z.-C., and Ma, J.-M.: Research on Dual-Variable Integrated Electro-Hydrostatic Actuator, Chinese J. Aeronaut., 19, 77–82, https://doi.org/10.1016/S1000-9361(11)60271-9, 2006. 5. Huang, L., Yu, T., Jiao, Z., and Li, Y.: Active Load-Sensitive Electro-Hydrostatic Actuator for More Electric Aircraft, Appl. Sci., 10, 6978, https://doi.org/10.3390/app10196978, 2020.
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