Electro-hydraulic load simulator (EHLS) is a typical closed-loop torque control system. It is used to simulate the load of aircraft actuator on ground hardware-in-the-loop simulation and experiments. In general, EHLS is fixed with actuator shaft together. Thus, the movement of actuator has interference torque named the surplus torque on the EHLS. The surplus torque is not only related to the velocity of the actuator movement, but also related to the frequency of actuator movement. Especially when the model of the actuator and EHLS is dissimilar, the surplus torque is obviously different on different frequencies. In order to eliminate the surplus torque for accurate load simulation, the actuator velocity input feedforword compensating method (AVIFC) is proposed in this paper. In this strategy, the actuator velocity synchronous signals are used for compensation of different frequency actuator movement to eliminate surplus torque on different frequencies. First, the mathematical model of EHLS and the actuator system is established. Based on the models, the AVIFC method is proposed. It reveals the reason that generates surplus torque on different frequencies of actuator. For verification, simulations and experiments are conducted to prove that the new strategy performs well against low, medium, and high frequency movement interference. The results show that this method can effectively suppress the surplus torque with different frequencies and improve precision of EHLS with actuator movement.
Skip Nav Destination
Article navigation
October 2018
Research-Article
Surplus Torque Elimination Control of Electro-Hydraulic Load Simulator Based on Actuator Velocity Input Feedforword Compensating Method
Zhihui Li,
Zhihui Li
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: lizhihui2013@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: lizhihui2013@buaa.edu.cn
Search for other works by this author on:
Yaoxing Shang,
Yaoxing Shang
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: syx@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: syx@buaa.edu.cn
Search for other works by this author on:
Zongxia Jiao,
Zongxia Jiao
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: zxjiao@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: zxjiao@buaa.edu.cn
Search for other works by this author on:
Shuai Wu,
Shuai Wu
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: ws@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: ws@buaa.edu.cn
Search for other works by this author on:
Jianyong Yao
Jianyong Yao
School of Mechanical Engineering,
Nanjing University of Science and Technology,
Nanjing 210094,
Jiangsu Province, China
e-mail: jerryyao.buaa@gmail.com
Nanjing University of Science and Technology,
Nanjing 210094,
Jiangsu Province, China
e-mail: jerryyao.buaa@gmail.com
Search for other works by this author on:
Zhihui Li
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: lizhihui2013@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: lizhihui2013@buaa.edu.cn
Yaoxing Shang
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: syx@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: syx@buaa.edu.cn
Zongxia Jiao
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: zxjiao@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: zxjiao@buaa.edu.cn
Shuai Wu
Science and Technology
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: ws@buaa.edu.cn
on Aircraft Control Laboratory,
School of Automation Science
and Electrical Engineering,
Beihang University,
Beijing 100191, China
e-mail: ws@buaa.edu.cn
Jianyong Yao
School of Mechanical Engineering,
Nanjing University of Science and Technology,
Nanjing 210094,
Jiangsu Province, China
e-mail: jerryyao.buaa@gmail.com
Nanjing University of Science and Technology,
Nanjing 210094,
Jiangsu Province, China
e-mail: jerryyao.buaa@gmail.com
1Corresponding author.
Contributed by the Dynamic Systems Division of ASME for publication in the JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT,AND CONTROL. Manuscript received April 1, 2016; final manuscript received February 22, 2018; published online May 2, 2018. Editor: Joseph Beaman.
J. Dyn. Sys., Meas., Control. Oct 2018, 140(10): 101001 (8 pages)
Published Online: May 2, 2018
Article history
Received:
April 1, 2016
Revised:
February 22, 2018
Citation
Li, Z., Shang, Y., Jiao, Z., Wu, S., and Yao, J. (May 2, 2018). "Surplus Torque Elimination Control of Electro-Hydraulic Load Simulator Based on Actuator Velocity Input Feedforword Compensating Method." ASME. J. Dyn. Sys., Meas., Control. October 2018; 140(10): 101001. https://doi.org/10.1115/1.4039663
Download citation file:
Get Email Alerts
Cited By
Robust Periodical Tracking for Fast Tool Servo Systems With Selective Disturbance Compensation
J. Dyn. Sys., Meas., Control (August 2022)
Feasibility of a Wearable Cold-Gas Thruster for Fall Prevention
J. Dyn. Sys., Meas., Control (August 2022)
Comparing Three Different Decoupling Control Approaches for Roll-To-Roll Printing Systems
J. Dyn. Sys., Meas., Control
Saturated Output Feedback Control for Robot Manipulators with Joints of Arbitrary Flexibility
J. Dyn. Sys., Meas., Control
Related Articles
Design and Simulation of Three Degrees-of-Freedom Tracking Systems for Capsule Endoscope
J. Dyn. Sys., Meas., Control (November,2016)
Erratum: “Design and Simulation of Three Degrees-of-Freedom Tracking Systems for Capsule Endoscope” [ASME J. Dyn. Syst., Meas., Control, 2016, 138(11), p. 111002; DOI: 10.1115/1.4033830 ]
J. Dyn. Sys., Meas., Control (July,2018)
Internal Model Control for Dynamic Systems With Preceded Backlash
J. Dyn. Sys., Meas., Control (March,2009)
A Modified Predictive Functional Control With Sliding Mode Observer for Automated Dry Clutch Control of Vehicle
J. Dyn. Sys., Meas., Control (June,2016)
Related Proceedings Papers
Related Chapters
New H∞ Controllers Design for Networked Control System with Disturbance Based on Asynchronous Dynamical System
International Conference on Advanced Computer Theory and Engineering (ICACTE 2009)
QP Based Encoder Feedback Control
Robot Manipulator Redundancy Resolution
Study of Metro Station Gathering and Distributing Capacity Based on Hybrid Petri Net
International Conference on Information Technology and Management Engineering (ITME 2011)