Get 20M+ Full-Text Papers For Less Than $1.50/day. Start a 14-Day Trial for You or Your Team.

Learn More →

Robust H2/H∞ DPDC dynamic output feedback controller for an uncertain tensor product model of statically unstable missile

Robust H2/H∞ DPDC dynamic output feedback controller for an uncertain tensor product model of... In this paper, the model filtering method is used to optimise the missile model. Based on the tensor product (TP) model transformation method, the uncertain TP model of the statically unstable missile is obtained and its robust variable gain mixed H2/H∞ performance dynamic parallel distributed compensation (DPDC) dynamic output feedback controller is designed. Firstly, the nonlinear model of statically unstable missile is optimised by model filtering method. The filtered missile model conforms to the actual engineering requirements, and meets the performance design requirements of H2. Then, the TP model transformation method is used to convert the nonlinear model of the statically unstable missile obtained after filtering into the TP model. Finally, the gain matrix of the robust variable gain mixed H2/H∞ performance dynamic output feedback controller is obtained by solving linear matrix inequalities (LMIs). The simulation results show that the designed DPDC dynamic output feedback controller. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png International Journal of Advanced Mechatronic Systems Inderscience Publishers

Robust H2/H∞ DPDC dynamic output feedback controller for an uncertain tensor product model of statically unstable missile

Loading next page...
 
/lp/inderscience-publishers/robust-h2-h-dpdc-dynamic-output-feedback-controller-for-an-uncertain-U5BpXNbYG1
Publisher
Inderscience Publishers
Copyright
Copyright © Inderscience Enterprises Ltd
ISSN
1756-8412
eISSN
1756-8420
DOI
10.1504/ijamechs.2023.128164
Publisher site
See Article on Publisher Site

Abstract

In this paper, the model filtering method is used to optimise the missile model. Based on the tensor product (TP) model transformation method, the uncertain TP model of the statically unstable missile is obtained and its robust variable gain mixed H2/H∞ performance dynamic parallel distributed compensation (DPDC) dynamic output feedback controller is designed. Firstly, the nonlinear model of statically unstable missile is optimised by model filtering method. The filtered missile model conforms to the actual engineering requirements, and meets the performance design requirements of H2. Then, the TP model transformation method is used to convert the nonlinear model of the statically unstable missile obtained after filtering into the TP model. Finally, the gain matrix of the robust variable gain mixed H2/H∞ performance dynamic output feedback controller is obtained by solving linear matrix inequalities (LMIs). The simulation results show that the designed DPDC dynamic output feedback controller.

Journal

International Journal of Advanced Mechatronic SystemsInderscience Publishers

Published: Jan 1, 2023

There are no references for this article.