Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness
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Publication:395166
DOI10.1007/s11071-010-9842-zzbMath1281.93029OpenAlexW1999060239MaRDI QIDQ395166
Publication date: 29 January 2014
Published in: Nonlinear Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s11071-010-9842-z
sliding mode controlfault tolerantattitude stabilizationinput constraintloss of actuator effectiveness
Variable mass, rockets (70P05) Adaptive or robust stabilization (93D21) Variable structure systems (93B12) Synthesis problems (93B50)
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Cites Work
- Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits
- Control of underactuated spacecraft with bounded inputs
- A backstepping-based low-and-high gain design for marine vehicles
- Adaptive control for nonlinear uncertain systems with actuator amplitude and rate saturation constraints
- Smooth sliding-mode control for spacecraft attitude tracking maneuvers
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