MATEC Web Conf.
Volume 309, 20202019 International Conference on Computer Science Communication and Network Security (CSCNS2019)
|Number of page(s)||9|
|Section||System Design and Optimization|
|Published online||04 March 2020|
Research on thrust vector control of nonlinear solid rocket motor nozzle based on active disturbance rejection technology
Beijing institute of precision electromechanical control equipment, Beijing, 100076 China
* Corresponding author: email@example.com
In this paper, based on the auto disturbance rejection control technology, the electromechanical servo system is used as the control actuator, and the thrust vector control of the solid rocket motor nozzle with typical nonlinear friction characteristics is studied and analyzed. In this paper, the realization of the classical PID algorithm and the lack of dynamic performance are analyzed, and then the compensation algorithm based on the auto disturbance rejection control technology is added. The algorithm compensates for the phase lag of the system due to the nonlinear friction characteristics. As a result, the frequency characteristics of the system have been significantly improved.
Key words: Auto disturbance rejection control technology / Non-linear load / Rocket nozzle / Thrust vector control
© The Authors, published by EDP Sciences, 2020
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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