Table of Contents Author Guidelines Submit a Manuscript
International Journal of Aerospace Engineering
Volume 2017, Article ID 5435090, 12 pages
Research Article

Networked Cascade Control System Design for Turboshaft Engines with Random Packet Dropouts

School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing, China

Correspondence should be addressed to Xiaofeng Liu; nc.ude.aaub@fxuil

Received 1 December 2016; Accepted 29 January 2017; Published 16 February 2017

Academic Editor: Wen Bao

Copyright © 2017 Xiaofeng Liu and Xu Sun. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


The distributed control architecture becomes more and more important in future gas turbine engine control systems, in which the sensors and actuators will be connected to the controllers via a network. Therefore, the control problem of network-enabled high-performance distributed engine control (DEC) has come to play an important role in modern gas turbine control systems, while, due to the properties of the network, the packet dropouts must be considered. This study introduces a distributed control system architecture based on a networked cascade control system (NCCS). Typical turboshaft engine distributed controllers are designed based on the NCCS framework with state feedback under random packet dropouts. The sufficient robust stable conditions are derived via the Lyapunov stability theory and linear matrix inequality approach. Simulations illustrate the effectiveness of the presented method.