Tracking Control of Vertical Tail Damaged Aircraft with dissimilar Actuator Configuration

被引：0

作者：

Ashraf, Muhammad Ammar ^{[1
]}

Ijaz, Salman ^{[2
]}

Zou, Yao ^{[1
]}

Ijaz, Hamdoon ^{[3
]}

机构：

[1] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing, Peoples R China

[2] Univ Nottingham, Dept Elect & Elect Engn, Ningbo, Peoples R China

[3] Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Engn, Beijing, Peoples R China

来源：

2021 IEEE INTERNATIONAL IOT, ELECTRONICS AND MECHATRONICS CONFERENCE (IEMTRONICS) | 2021年

关键词：

linear matrix inequality; control reconfiguration; virtual actuator; linear quadratic regulator; FAULT-TOLERANT CONTROL; DESIGN;

D O I：

10.1109/IEMTRONICS52119.2021.9422581

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This article presents a new control scheme for an aircraft that has suffered from actuator failure due to severe damage to its vertical tail. The damaged degree of the vertical tail is treated as uncertainty. Firstly an output feedback controller is designed for the nominal lateral dynamic model of aircraft. However, when the actuator's fault/failure occurs, the idea of generalized virtual actuators is adopted. In this way, the same baseline controller is used even in the presence of fault/failure. Linear matrix inequality is used to compute the controller and virtual actuator's gains. The simulation results show good tracking performance and fault-tolerant competency.

引用

页码：514 / 519

页数：6

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