Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications

Joint Authors

Hou, Chuanjing
Hu, Lisheng
Zhang, Yingwei

Source

Mathematical Problems in Engineering

Issue

Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-14, 14 p.

Publisher

Hindawi Publishing Corporation

Publication Date

2015-05-21

Country of Publication

Egypt

No. of Pages

14

Main Subjects

Civil Engineering

Abstract EN

An adaptive failure compensation scheme using output feedback is proposed for a class of nonlinear systems with nonlinearities depending on the unmeasured states of systems.

Adaptive high-gain K-filters are presented to suppress the nonlinearities while the proposed backstepping adaptive high-gain controller guarantees the stability of the closed-loop system and small tracking errors.

Simulation results verify that the adaptive failure compensation scheme is effective.

American Psychological Association (APA)

Hou, Chuanjing& Hu, Lisheng& Zhang, Yingwei. 2015. Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications. Mathematical Problems in Engineering،Vol. 2015, no. 2015, pp.1-14.
https://search.emarefa.net/detail/BIM-1073589

Modern Language Association (MLA)

Hou, Chuanjing…[et al.]. Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications. Mathematical Problems in Engineering No. 2015 (2015), pp.1-14.
https://search.emarefa.net/detail/BIM-1073589

American Medical Association (AMA)

Hou, Chuanjing& Hu, Lisheng& Zhang, Yingwei. Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications. Mathematical Problems in Engineering. 2015. Vol. 2015, no. 2015, pp.1-14.
https://search.emarefa.net/detail/BIM-1073589

Data Type

Journal Articles

Language

English

Notes

Includes bibliographical references

Record ID

BIM-1073589