Transactions of Nanjing University of Aeronautics & Astronautics
Research and Design of Coordinated Control Strategy for Smart Electromechanical Actuator System
- Article
- Figures
- Metrics
- Preview PDF
- Reference
- Related
- Cited by
- Materials
Abstract:
In order to improve the frequency response and anti-interference characteristics of the smart electromechanical actuator（EMA） system， and aiming at the force fighting problem when multiple actuators work synchronously， a multi input multi output （MIMO） position difference cross coupling control coordinated strategy based on double-closed-loop load feedforward control is proposed and designed. In this strategy， the singular value method of return difference matrix is used to design the parameter range that meets the requirements of system stability margin， and the sensitivity function and the H∞ norm theory are used to design and determine the optimal solution in the obtained parameter stability region， so that the multi actuator system has excellent synchronization， stability and anti-interference. At the same time， the mathematical model of the integrated smart EMA system is established. According to the requirements of point-to-point control， the controller of double-loop control and load feedforward compensation is determined and designed to improve the frequency response and anti-interference ability of single actuator. Finally， the 270 V high-voltage smart EMA system experimental platform is built， and the frequency response， load feedforward compensation and coordinated control experiments are carried out to verify the correctness of the position difference cross coupling control strategy and the rationality of the parameter design， so that the system can reach the servo control indexes of bandwidth 6 Hz， the maximum output force 20 000 N and the synchronization error ≤0.1 mm， which effectively solves the problem of force fighting.
Keywords:
Project Supported:
This work was supported by the National Natural Science Foundation of China （No.52077100） and the Aviation Science Foundation （No.201958052001）.
Clc Number:
V11
Mobile website
