Terminal sliding mode control with unidirectional auxiliary surfaces for hypersonic vehicles based on adaptive disturbance observer

DOI10.1155/2015/285716zbMath1394.93230OpenAlexW1699145473WikidataQ59117857 ScholiaQ59117857MaRDI QIDQ1665233

Bin Jiang, Naibao He, Qian Gao, Chang-Sheng Jiang

Publication date: 27 August 2018

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2015/285716

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable structure systems (93B12)

Cites Work

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• Composite disturbance-observer-based control and H _∞ control for complex continuous models
• A state-dependent boundary layer design for sliding mode control
• Attitude control of reusable launch vehicle in reentry phase with input constraint via robust adaptive backstepping control

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