Robust attitude tracking for rigid spacecraft with prescribed transient performance

DOI10.1080/00207179.2016.1250955zbMath1380.93100OpenAlexW2537425617MaRDI QIDQ3132993

Unnamed Author, Zhigang Zhou, Di Zhou, Yongan Zhang

Publication date: 12 February 2018

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179.2016.1250955

zbMATH Keywords

transient performanceattitude trackinguncertain dynamicsbounded disturbancesrigid spacecraft

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

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Event-triggered integral sliding mode controller for rigid spacecraft attitude tracking with angular velocity constraint ⋮ Fault‐tolerant control of an aerial manipulator with guaranteed tracking performance ⋮ Observer-based hybrid control for global attitude tracking onSO(3) with input quantisation ⋮ Output regulation problem with prescribed performance for nonlinear lower-triangular system ⋮ Fixed-time control for high-precision attitude stabilization of flexible spacecraft ⋮ Chebyshev neural network-based attitude-tracking control for rigid spacecraft with finite-time convergence ⋮ Flexible performance-based adaptive fault-tolerant attitude tracking control for input-constrained satellite ⋮ Prescribed performance fixed-time tracking control for a class of second-order nonlinear systems with disturbances and actuator saturation

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