Neural‐network‐based adaptive finite‐time output constraint control for rigid spacecrafts
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Publication:6085216
DOI10.1002/rnc.5766zbMath1527.93231OpenAlexW3197693197MaRDI QIDQ6085216
Liang Tao, Qiang Chen, Unnamed Author, Unnamed Author
Publication date: 2 December 2023
Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/rnc.5766
Adaptive control/observation systems (93C40) Orbital mechanics (70M20) Finite-time stability (93D40)
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Cites Work
- Unnamed Item
- A low-complexity global approximation-free control scheme with prescribed performance for unknown pure feedback systems
- Finite-time command filtered backstepping control for a class of nonlinear systems
- Adaptive fuzzy finite-time fault-tolerant attitude control of rigid spacecraft
- Chattering-free full-order recursive sliding mode control for finite-time attitude synchronization of rigid spacecraft
- Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
- Funnel Control With Saturation: Nonlinear SISO Systems $ $
- Finite‐time attitude‐tracking control for rigid spacecraft with actuator failures and saturation constraints
- Adaptive Asymptotic Tracking With Global Performance for Nonlinear Systems With Unknown Control Directions
- Adaptive reliable guaranteed performance control of uncertain nonlinear systems by using exponent‐dependent barrier Lyapunov function
- Robust stabilization of spacecraft attitude motion under magnetic control through time‐varying integral sliding mode
- Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques
- Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization
- Finite-time spacecraft attitude control under input magnitude and rate saturation
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