Finite-time spacecraft attitude control under input magnitude and rate saturation
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Publication:6166382
DOI10.1007/s11071-019-05388-6zbMath1516.93195OpenAlexW2990714555WikidataQ126658624 ScholiaQ126658624MaRDI QIDQ6166382
Anton H. J. de Ruiter, An-Min Zou, Krishna Dev Kumar
Publication date: 2 August 2023
Published in: Nonlinear Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s11071-019-05388-6
Automated systems (robots, etc.) in control theory (93C85) Orbital mechanics (70M20) Finite-time stability (93D40)
Related Items (5)
Synchronous control of multiple electrohydraulic actuators under distributed switching topologies with lumped uncertainty ⋮ Finite‐time fault‐tolerant output feedback attitude control of spacecraft formation with guaranteed performance ⋮ Neural‐network‐based adaptive finite‐time output constraint control for rigid spacecrafts ⋮ Optimal non-fragile control design for linear systems under amplitude and rate saturation: an LMI approach ⋮ Asymmetric integral barrier Lyapunov function-based adaptive tracking control considering full-state with input magnitude and rate constraint
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