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

المؤلفون المشاركون

Liu, Xiaofeng
Sun, Xu

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2017، العدد 2017 (31 ديسمبر/كانون الأول 2017)، ص ص. 1-12، 12ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2017-02-16

دولة النشر

مصر

عدد الصفحات

12

الملخص EN

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.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Liu, Xiaofeng& Sun, Xu. 2017. H ∞ Networked Cascade Control System Design for Turboshaft Engines with Random Packet Dropouts. International Journal of Aerospace Engineering،Vol. 2017, no. 2017, pp.1-12.
https://search.emarefa.net/detail/BIM-1158118

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Liu, Xiaofeng& Sun, Xu. H ∞ Networked Cascade Control System Design for Turboshaft Engines with Random Packet Dropouts. International Journal of Aerospace Engineering No. 2017 (2017), pp.1-12.
https://search.emarefa.net/detail/BIM-1158118

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Liu, Xiaofeng& Sun, Xu. H ∞ Networked Cascade Control System Design for Turboshaft Engines with Random Packet Dropouts. International Journal of Aerospace Engineering. 2017. Vol. 2017, no. 2017, pp.1-12.
https://search.emarefa.net/detail/BIM-1158118

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1158118