Attitude tracking control of spacecraft with preset‐time preset‐bounded convergence
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Publication:6180529
DOI10.1002/rnc.6369zbMath1529.93014MaRDI QIDQ6180529
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Publication date: 19 December 2023
Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)
Cites Work
- Finite-time attitude control for rigid spacecraft subject to actuator saturation
- Homogeneous Lyapunov function for homogeneous continuous vector field
- Time-varying feedback for regulation of normal-form nonlinear systems in \textit{prescribed} finite time
- Fixed-time attitude tracking control for rigid spacecraft
- Attitude control of rigid spacecraft with predefined-time stability
- Coupled orbit-attitude dynamics and trajectory tracking control for spacecraft electromagnetic docking
- Practical fixed-time consensus for integrator-type multi-agent systems: a time base generator approach
- Finite-time and fixed-time stabilization: implicit Lyapunov function approach
- Adaptive attitude tracking control for rigid spacecraft with finite-time convergence
- Finite-time angular velocity observers for rigid-body attitude tracking with bounded inputs
- The attitude control problem
- Homogeneous Approximation, Recursive Observer Design, and Output Feedback
- Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization
- Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems
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