Nonlinear robust control for reusable launch vehicles in reentry phase based on time-varying high order sliding mode

DOI10.1016/j.jfranklin.2013.04.022zbMath1392.93007OpenAlexW2021744908WikidataQ56925758 ScholiaQ56925758MaRDI QIDQ1659382

Bailing Tian, Fang Wang, Qun Zong, Wenru Fan, Jie Wang

Publication date: 15 August 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.2013.04.022

zbMATH Keywords

algebraic equationsreusable launch vehicleshigh order sliding mode attitude controllernonlinear robust controllertime-varying sliding mode manifold

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Variable structure systems (93B12)

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Multivariable uniform finite-time output feedback reentry attitude control for RLV with mismatched disturbance, PID pitch attitude control for unstable flight vehicle in the presence of actuator delay: tuning and analysis, A fixed-time output feedback control scheme for double integrator systems, Finite‐time attitude tracking control and vibration suppression for flexible spacecraft, Robust fault accommodation strategy of the reentry vehicle: a disturbance estimate-triggered approach, Adaptive-gain multivariable super-twisting sliding mode control for reentry RLV with torque perturbation, Gradient method using pseudospectral collocation scheme for two-stage optimal control with an unspecified switching time

Cites Work

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