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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Proceedings ArticleDOI
Continuous Integral Terminal Sliding Mode Control for a Class of Uncertain Nonlinear Systems
Huawei Niu,Qixun Lan +1 more
TL;DR: A finite-time disturbance observer based ITSMC law is proposed, strict theoretical analysis shows that the composite ITSMC approach can eliminate chattering completely without losing disturbance attenuation ability and performance robustness of ITSMC.
Journal Article
State-of-the-art in Comprehensive Cascade Control Approach through Monte-Carlo Based Representation
TL;DR: It is to note that the new insights in the area of the research’s topic are valuable to outperform a class of spacecrafts performance as the realizations of the acquired results are to be addressed in both real and academic environments.
Proceedings ArticleDOI
Relative position fixed-time tracking control of spacecraft
Wei Chen,Qinglei Hu,Lei Guo +2 more
TL;DR: In this article, a fixed-time sliding mode control scheme in conjunction with a time-varying sliding mode surface is proposed to achieve the relative motion tracking of leader-follower spacecraft within the allotted time.
Proceedings ArticleDOI
Trajectory Tracking of Unmanned Surface Vehicle based on Terminal Sliding Mode
TL;DR: In this article , a sliding mode controller (SMC) with nonsingular terminal method was proposed to reject the external disturbance, and a disturbance observer (DO) was designed to improve the accuracy of the trajectory tracking.
Journal ArticleDOI
Finite-Time Attitude Cooperative Control of Multiple Unmanned Aerial Vehicles via Fast Nonsingular Terminal Sliding Mode Control
TL;DR: In this paper , a distributed fast nonsingular terminal sliding mode control (FNTSMC) is used with quaternion-description dynamical systems for attitude cooperative control of multiple UAVs with unknown dynamics and external disturbances.
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.