基于反馈线性化和PID的航空气动系统温度控制

22nd Mediterranean Conference on Control and Automation Pub Date : 2014-06-16 DOI:10.1109/MED.2014.6961495

D. Silva, Wallace Turcio, E. Tannuri

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引用次数: 12

摘要

本文提出了一个航空气动系统的简化非线性模型。提出了一种采用反馈线性化理论与PID相结合的系统温度控制设计方法。给出并讨论了用Matlab/Simulink®进行的仿真结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Temperature control of an aeronautical pneumatic system using feedback linearization and PID

This work presents a simplified nonlinear model for an aeronautical pneumatic system. A methodology for designing the system temperature control is proposed using the feedback linearization theory combined with a PID. Simulation results performed with Matlab/Simulink® are presented and discussed.

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22nd Mediterranean Conference on Control and Automation

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