Servo system controller of rocket engine based on Characteristic model

被引：0

作者：

Fan, Yao ^{[1
]}

Li, Liang ^{[2
]}

Qi, Peng ^{[3
]}

Ren, Zhang ^{[1
]}

Wang, Yuan-Zhi ^{[4
]}

机构：

[1] Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing, China

[2] Shanghai Electro-Mechanical Engineering Institute, Shanghai, China

[3] The Second Artillery Representative Office in the Fourth Academy of CASC, Xi'an, China

[4] Unit 96630, The Chinese People's Liberation Army, Beijing, China

来源：

Guti Huojian Jishu/Journal of Solid Rocket Technology | 2015年 / 38卷 / 01期

关键词：

Optimization - Rocket engines - Adaptive control systems - Parameter estimation - Rockets - Controllers - Evolutionary algorithms - Uncertainty analysis - Control theory;

D O I：

10.7673/j.issn.1006-2793.2015.01.028

中图分类号：

学科分类号：

摘要：

Servo system controller based on characteristic model was proposed for the new high-thrust rocket engine. Firstly, the characteristic modeling method was introduced and the range of parameters was discussed. Secondly, artificial bee colony algorithm was employed to estimate the characteristic model parameters of servo system in real time under the condition of equivalent output of characteristic model and actual system. Finally, golden section adaptive control law was introduced to stabilize the close-loop system in the process of parameters estimation, feedforward tracking control law, logical integral and logical derivative control law were also used to improve the performance of servo system. Simulation results demonstrate that the servo system controller can guarantee the accurate tracking of command and robustness to model uncertainty. ©, 2015, Journal of Solid Rocket Technology. All right reserved.

引用

页码：145 / 150

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