Robust Actuator‐Fault‐Tolerant Control System Based on Sliding‐Mode Observer for Thrust‐Vectoring Aircrafts-Reference-Cited by-同舟云学术

Robust Actuator‐Fault‐Tolerant Control System Based on Sliding‐Mode Observer for Thrust‐Vectoring Aircrafts

Published:2018-06-22 Issue:1 Volume:21 Page:236-247
ISSN:1561-8625
Container-title:Asian Journal of Control
language:en
Short-container-title:Asian Journal of Control

Author:

Li Bingqian¹^ORCID,Dong Wenhan¹,Xiong Chao¹

Affiliation:

1. Air Force Engineering University

Publisher

Wiley

Subject

Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/asjc.1841

Reference33 articles.

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2. Research on dynamic control allocation method for aircraft with thrust vector;Zhang H. X.;Electron. Optics Control,2016

3. High‐alpha flight maneuverability enhancement of a twin engine fighter‐bomber aircraft for air combat superiority using thrust‐vectoring control;Ozgur A.;AIAA Guid. Navig. Control Conf.,2007

4. Dynamic characteristics and challenges for control system of super‐maneuverable aircraft;Zhu J. H.;J. Control Theor. Appl.,2014

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