Multivariable uniform finite-time output feedback reentry attitude control for RLV with mismatched disturbance

DOI10.1016/J.JFRANKLIN.2018.01.042zbMath1390.93333OpenAlexW2789730491WikidataQ130097173 ScholiaQ130097173MaRDI QIDQ1643213

Bailing Tian, Qun Zong, Hanchen Lu, Zongyu Zuo

Publication date: 19 June 2018

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2018.01.042

zbMATH Keywords

output feedback controlbi-limit homogeneous techniquecontinuous multivariable uniform finite-time output feedback reentry attitude controlfinite-time controllerreusable launch vehicle (RLV)robust sliding mode differentiatoruniform finite-time stability

Mathematics Subject Classification ID

Feedback control (93B52) Variable mass, rockets (70P05) Variable structure systems (93B12) Robust stability (93D09)

Related Items (6)

Adaptive fault-tolerant attitude control for hypersonic reentry vehicle subject to complex uncertainties ⋮ Tackling mismatched uncertainty in robust constraint-following control of underactuated systems ⋮ Anti-disturbance control for HVs system subject to nonlinear actuator characteristics with extended state observer ⋮ Event-triggered-based adaptive super-twisting attitude tracking for RLV in reentry phase ⋮ Modeling and switching control of air-breathing hypersonic vehicle with variable geometry inlet ⋮ Fast finite-time tracking control for multi-agent systems with mismatched disturbances under directed communication graphs

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