Adaptive actuator failure compensation control for hypersonic vehicle with full state constraints-Reference-Cited by-同舟云学术

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Adaptive actuator failure compensation control for hypersonic vehicle with full state constraints

Published:2019-02 Issue: Volume:85 Page:464-473
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xi Yong,Meng Yao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Adaptive fault-tolerant attitude tracking control of spacecraft with prescribed performance;Hu;IEEE/ASME Trans. Mechatron.,2018

2. Output feedback back-stepping control for a generic hypersonic vehicle via small-gain theorem;Zong;Aerosp. Sci. Technol.,2012

3. Continuous higher order sliding mode control with adaptation of air breathing hypersonic missile;Yu;Int. J. Adapt. Control Signal Process.,2016

4. Spacecraft attitude fault-tolerant control based on iterative learning observer and control allocation;Hu;Aerosp. Sci. Technol.,2018

5. Global neural dynamic surface tracking control of strict-feedback systems with application to hypersonic flight vehicle;Xu;IEEE Trans. Neural Netw. Learn. Syst.,2015

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