Attitude control of rigid spacecraft with predefined-time stability
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Publication:2181338
DOI10.1016/j.jfranklin.2020.01.001zbMath1437.93097OpenAlexW3007327131MaRDI QIDQ2181338
Chaoyong Li, Yue Miao, Feng Wang, Inseok Hwang
Publication date: 19 May 2020
Published in: Journal of the Franklin Institute (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jfranklin.2020.01.001
Application models in control theory (93C95) Variable structure systems (93B12) Stability of control systems (93D99)
Related Items (11)
Preassigned-time projective synchronization of delayed fully quaternion-valued discontinuous neural networks with parameter uncertainties ⋮ Predefined‐time backstepping control for a nonlinear strict‐feedback system ⋮ On event‐triggered nonsmooth attitude tracking controller for a rigid spacecraft ⋮ Predefined‐time tracking control for high‐order nonlinear systems with control saturation ⋮ Continuous precise predefined-time attitude tracking control for a rigid spacecraft ⋮ Barrier function-based prescribed-performance adaptive attitude tracking control for spacecraft with uncertainties ⋮ Attitude tracking control of spacecraft with preset‐time preset‐bounded convergence ⋮ Predefined‐time guaranteed performance attitude takeover control for non‐cooperative spacecraft with uncertainties ⋮ Barrier Lyapunov function-based adaptive fuzzy attitude tracking control for rigid satellite with input delay and output constraint ⋮ Predefined-time control for free-floating space robots in task space ⋮ Practical predefined-time attitude coordination control for multiple rigid spacecraft
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