Two-layer terminal sliding mode attitude control of satellites equipped with reaction wheels
From MaRDI portal
Publication:6563344
DOI10.1002/asjc.1878MaRDI QIDQ6563344
Farhad Bayat, Mojtaba Javaheri
Publication date: 27 June 2024
Published in: Asian Journal of Control (Search for Journal in Brave)
finite-time controlterminal sliding mode controlsatellite attitude controlunknown disturbancesreaction wheels
Cites Work
- Fully magnetic attitude control for spacecraft subject to gravity gradient
- Sliding mode observers for detection and reconstruction of sensor faults
- Control Lyapunov function optimal sliding mode controllers for attitude tracking of spacecraft
- Adaptive attitude tracking control for rigid spacecraft with finite-time convergence
- Nonlinear Analysis and Attitude Control of a Gyrostat Satellite with Chaotic Dynamics Using Discrete-Time LQR-OGY
- Finite-time angular velocity observers for rigid-body attitude tracking with bounded inputs
- Robust attitude tracking control of flexible spacecraft for achieving globally asymptotic stability
- Global finite-time attitude stabilization for rigid spacecraft in the exponential coordinates
- Spacecraft Anti‐Unwinding Attitude Control Using Second‐Order Sliding Mode
- Three‐Axis Global Magnetic Attitude Control of Earth‐Pointing Satellites in Circular Orbit
- Adaptive fault‐tolerant attitude tracking control for spacecraft formation with unknown inertia
- Finite-Time Stability of Continuous Autonomous Systems
- Finite‐time attitude stabilization for rigid spacecraft
- Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization
- Optimal Output Feedback Controllers for Spacecraft Attitude Tracking
Related Items (2)
Attitude tracking of rigid bodies using exponential coordinates and a disturbance observer ⋮ Finite-time adaptive fault-tolerant control for rigid spacecraft attitude tracking
This page was built for publication: Two-layer terminal sliding mode attitude control of satellites equipped with reaction wheels
