Journal ArticleDOI
Adaptive attitude tracking control for rigid spacecraft with finite-time convergence
Kunfeng Lu,Yuanqing Xia +1 more
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TLDR
The proposed FNTSM control laws (FNTSMCLs) by employing FNTSMS associated with adaptation provide finite-time convergence, robustness, faster, higher control precision, and they are chattering-free.About:
This article is published in Automatica.The article was published on 2013-12-01. It has received 425 citations till now. The article focuses on the topics: Sliding mode control & Adaptive control.read more
Citations
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Fault-tolerant control for full-state error constrained attitude tracking of uncertain spacecraft
TL;DR: In this paper , a saturated adaptive robust fault-tolerant control (FTC) algorithm is proposed, which can eliminate the uniform strong controllability (USC) assumption without requiring the multiplicative actuator faults to be differentiable.
Journal ArticleDOI
Robust attitude tracking control of spacecraft under unified actuator dynamics
TL;DR: In this paper , a robust attitude tracking control scheme is proposed by incorporating a disturbance observer and an auxiliary dynamic system into the command filtered backstepping control design, which can guarantee the attitude tracking errors converge to the arbitrary small neighbourhood of zero even subject to actuator dynamics.
Journal ArticleDOI
Fuzzy Adaptive Finite Time Command Filter Backstepping Control of Power System
TL;DR: It is proven that the designed controller ensures the rotor power angle in the power system converge to the expected value and all variables of the control systems are semi-global practical finite-time stable (SGPFS).
Journal ArticleDOI
Multiple Model Adaptive Attitude Control of LEO Satellite with Angular Velocity Constraints
TL;DR: An adaptive output feedback control law is proposed for attitude control under angular velocity constraints and its almost global asymptotic stability is proved.
Journal ArticleDOI
Constrained Nonsingular Terminal Sliding Mode Attitude Control for Spacecraft: A Funnel Control Approach
TL;DR: In this article , an adaptive constrained attitude control for uncertain spacecraft is proposed, which is based on the concept of nonsingular terminal sliding mode control and funnel control for nonlinear systems, and analytically proved that the system trajectories converge to an arbitrary small region around the origin within a fixed time.
References
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Journal ArticleDOI
Continuous finite-time control for robotic manipulators with terminal sliding modes
TL;DR: A continuous finite-time control scheme for rigid robotic manipulators is proposed using a new form of terminal sliding modes using the Lyapunov stability theory, and theoretical analysis and simulation results show that faster and high-precision tracking performance is obtained.
Journal ArticleDOI
Brief Non-singular terminal sliding mode control of rigid manipulators
Yong Feng,Xinghuo Yu,Zhihong Man +2 more
TL;DR: This paper presents a global non-singular terminal sliding mode controller for rigid manipulators to enable the elimination of the singularity problem associated with conventional terminal slide mode control.
Book
Space Vehicle Dynamics and Control
TL;DR: Space Vehicle Dynamics and Control, Second Edition as discussed by the authors provides a solid foundation in dynamic modeling, analysis, and control of space vehicles featuring detailed sections covering the fundamentals of controlling orbital, attitude, and structural motions.
Journal ArticleDOI
Attitude stabilization of rigid spacecraft with finite‐time convergence
TL;DR: In this article, two sliding mode controllers are proposed to force the state variables of the closed-loop system to converge to the origin in finite time, and the second control design consists of the estimation of the uncertainty and disturbance by adaptive method and thus it achieves the decrease of undesired chattering effectively.
Journal ArticleDOI
Fast terminal sliding-mode control design for nonlinear dynamical systems
Xinghuo Yu,Man Zhihong +1 more
TL;DR: A fast terminal dynamics is proposed and used in the design of the sliding-mode control for single-input single-output nonlinear dynamical systems.