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
Adaptive SMC-based Trajectory Tracking Control of Underactuated Overhead Cranes
TL;DR: An adaptive version of anti-sway trajectory tracking controller for overhead cranes is developed that achieves precise positioning and swing suppression despite input saturation, system uncertainty and external disturbances.
Journal ArticleDOI
Immersion and invariance sliding mode control with time-delay estimation for rigid spacecraft with uncertainties and actuator faults
TL;DR: In this paper , an immersion and invariance sliding mode control with time-delay estimation (IISMCTDE) is proposed to cope with uncertainties, disturbances, and actuator faults.
Proceedings ArticleDOI
Model Reference Adaptive Control Design for CubeSat with Magnetorquer
TL;DR: In this paper , the Model Reference Adaptive Control (MRAC) design for the CubeSat 1U prototype with a magnetorquer to control the yaw angle was proposed.
Journal ArticleDOI
Spacecraft attitude estimation under attitude tracking maneuver during close-proximity operations
Daero Lee,Sergio Gallucci +1 more
TL;DR: In this paper , a real-time relative three-axis attitude estimation using a camera and two gyros under momentum changes during close-proximity operations is presented. But the camera sensor provides quaternion measurements that relate the body frame of the deputy spacecraft with respect to the body frames of the chief spacecraft.
Journal ArticleDOI
Antiunwinding Sliding Mode Control for Rigid Spacecraft Based on Modified Rodrigues Parameters
TL;DR: In this paper , a sliding mode controller is developed to ensure that the sliding surface is reachable, and a dynamic parameter is designed to guarantee unwinding-free performance of the closed-loop system when the system states are outside the sliding surfaces.
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.