Continuous higher order sliding mode control with adaptation of air breathing hypersonic missile

DOI10.1002/ACS.2664zbMath1348.93073OpenAlexW2416522837WikidataQ57915471 ScholiaQ57915471MaRDI QIDQ2829484

Christopher Edwards, Polk Yu, Yuri B. Shtessel

Publication date: 28 October 2016

Published in: International Journal of Adaptive Control and Signal Processing (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/10871/19109

zbMATH Keywords

adaptive controlhigher order sliding mode controlhypersonic missile control

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95) Adaptive control/observation systems (93C40) Variable structure systems (93B12) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (5)

Disturbance observer-based robust missile autopilot design with full-state constraints via adaptive dynamic programming ⋮ Zero-sum differential games-based fast adaptive robust optimal sliding mode control design for uncertain missile autopilot with constrained input ⋮ Multivariable variable-gain super-twisting control via output feedback for systems with arbitrary relative degrees ⋮ From adaptive control to variable structure systems - seeking harmony ⋮ Adaptive high order sliding mode controller/observer based terminal sliding mode for MIMO uncertain nonlinear system

Cites Work

• Adaptive sliding mode tracking control for a flexible air-breathing hypersonic vehicle
• Adaptive sliding mode control with application to super-twist algorithm: equivalent control method
• Geometric homogeneity with applications to finite-time stability
• Adaptive sliding mode control and observation
• Sliding order and sliding accuracy in sliding mode control
• Higher-order sliding modes, differentiation and output-feedback control
• Quasi-continuous high-order sliding-mode controllers

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