摘要
Future gas turbine engine control systems will be based on distributed architecture, in which, the sensors and actuators will be connected to the controllers via a communication network. The performance of the distributed engine control (DEC) is dependent on the network performance. 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 a H∞ output feedback under network-induced time delays and uncertain disturbances. The sufficient conditions for robust stability are derived via the Lyapunov stability theory and linear matrix inequality approach. Both numerical and hardware-in-loop simulations illustrate the effectiveness of the presented method.
| 源语言 | 英语 |
|---|---|
| 期刊论文编号 | e0163545 |
| 期刊 | PLOS ONE |
| 卷 | 11 |
| 期 | 9 |
| DOI | |
| 出版状态 | 已出版 - 9月 2016 |
学术指纹
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