Force tracking control of an electro-hydraulic control loading system on a flight simulator using inverse model control and a damping compensator

Author:

Zhao Jinsong12,Shen Gang34,Zhu Weidong4,Yang Chifu5,Agrawal Sunil K6

Affiliation:

1. Key Laboratory of Advanced Forging & Stamping Technology and Science (Yanshan University), Ministry of Education of China, China

2. Hebei Provincial Key Laboratory of Heavy Machinery Fluid Power Transmission and Control, Yanshan University, China

3. School of Mechatronic Engineering, China University of Mining and Technology, China

4. Department of Mechanical Engineering, University of Maryland, Baltimore County, USA

5. State Key Laboratory of Robotics and System of China, Harbin Institute of Technology, China

6. Department of Mechanical Engineering, Columbia University, USA

Abstract

The electro-hydraulic control loading system (EHCLS) of a flight simulator is mainly used to simulate the force feel of flying a real airplane. A double-loop model, including control and hydraulic mechanism of the EHCLS, is established and its force–displacement impedance is analysed to evaluate force tracking performances and its stability. An approximated feed-forward inverse model controller is designed using a zero phase error compensation method for expanding the frequency bandwidth of the inner loop because the identified force closed-loop model is a nonminimum phase system and its direct inverse model is unstable. Modelling error between the designed feed-forward inverse model and the actual plant is discussed and a damping compensator is presented to increase stability of the EHCLS. Theoretical analysis, simulation and experimental results show that the control methods presented are feasible and can effectively improve force feel fidelity and stability of the EHCLS.

Funder

the Projects supported by Independent Study Program for Young teachers in Yanshan University

National Natural Science Foundation of China

Publisher

SAGE Publications

Subject

Instrumentation

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