Sliding Mode Differentiator Based Tracking Control of Uncertain Nonlinear Systems with Application to Hypersonic Flight-Reference-Cited by-同舟云学术

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Sliding Mode Differentiator Based Tracking Control of Uncertain Nonlinear Systems with Application to Hypersonic Flight

Published:2018-11-18 Issue:1 Volume:21 Page:143-155
ISSN:1561-8625
Container-title:Asian Journal of Control
language:en
Short-container-title:Asian Journal of Control

Author:

An Hao¹^ORCID,Fidan Baris²^ORCID,Wu Qianqian³^ORCID,Wang Changhong¹^ORCID,Cao Xibin⁴

Affiliation:

1. Space Control and Inertial Technology Research CenterHarbin Institute of Technology Harbin 150001 China

2. Department of Mechanical and Mechatronics EngineeringUniversity of Waterloo Waterloo ON N2L 3G1 Canada

3. Center for Composite Materials and StructuresHarbin Institute of Technology Harbin 150001 China

4. Research Center of Satellite TechnologyHarbin Institute of Technology Harbin 150001 China

Funder

China Postdoctoral Science Foundation

Publisher

Wiley

Subject

Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/asjc.1932

Reference29 articles.

1. Command Filtered Backstepping

2. Command Filtered Adaptive Backstepping

3. Fault-tolerant control using command-filtered adaptive back-stepping technique: Application to hypersonic longitudinal flight dynamics

4. Adaptive Actuator Failure Compensation for a Class of Nonlinear Systems With Unknown Control Direction

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4. Adaptive fault‐tolerant control for a class of flexible air‐breathing hypersonic vehicles;Asian Journal of Control;2023-03-19

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