Observer-based continuous finite-time attitude control for rigid–flexible coupling satellites
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Publication:5240713
DOI10.1080/00207179.2018.1458155zbMath1425.93070OpenAlexW2802726623WikidataQ130051508 ScholiaQ130051508MaRDI QIDQ5240713
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Publication date: 29 October 2019
Published in: International Journal of Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/00207179.2018.1458155
finite-time controlextended state observerrigid-flexible coupling spacecraftnon-singular terminal sliding modefast power reaching lawrapid manoeuver
Application models in control theory (93C95) Observability (93B07) Variable structure systems (93B12)
Related Items (2)
Agile attitude maneuver with active vibration-suppression for flexible spacecraft ⋮ Inertia‐free attitude stabilization for flexible spacecraft with active vibration suppression
Cites Work
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- Dynamic modelling and control of a rotating Euler–Bernoulli beam
- Nonsingular fast terminal sliding-mode control for nonlinear dynamical systems
- Continuous finite-time stabilization of the translational and rotational double integrators
- A new synthesis method for uncertain systems the Self-Stable Region approach
- Fast terminal sliding-mode control design for nonlinear dynamical systems
- Adaptive robust attitude control of a flexible spacecraft
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