h∞ networked cascade control system design for turboshaft engines with random packet dropouts

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ID: 133821
2017
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Abstract
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 H∞ 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.
Reference Key
liu2017internationalh Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;Xiaofeng Liu;Xu Sun
Journal shanghai kou qiang yi xue = shanghai journal of stomatology
Year 2017
DOI
10.1155/2017/5435090
URL
http://dx.doi.org/10.1155/2017/5435090
Keywords
motor vehicles astronautics aeronautics

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