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Journal ArticleDOI

Adaptive attitude tracking control for rigid spacecraft with finite-time convergence

Kunfeng Lu, +1 more
- 01 Dec 2013 - 
- Vol. 49, Iss: 12, pp 3591-3599
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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.

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Citations
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Journal ArticleDOI

High-Performance Adaptive Attitude Control of Spacecraft With Sliding Mode Disturbance Observer

- 01 Jan 2022 - 
TL;DR: In this paper , a sliding mode disturbance observer (SMDO) is designed to address the attitude tracking problem of rigid-body spacecraft in the presence of external disturbances and parameter uncertainties, and a special adaptive integral sliding mode controller is combined with the SMDO to ensure system state convergence.
Proceedings ArticleDOI

Adaptive Fast Non-singular Terminal Sliding Mode Control for Robotic Manipulators with Deadzone

TL;DR: An adaptive chattering-free fast non-singular terminal sliding mode (CFNTSM) control approach for the trajectory tracking of robotic manipulators system with deadzone is proposed and simulation results validate the effectiveness of the proposed control strategy.
Journal ArticleDOI

Nonlinear Adaptive Line-of-Sight Path Following Control of Unmanned Aerial Vehicles considering Sideslip Amendment and System Constraints

TL;DR: A new nonlinear path following scheme integrated with a heading control law for achieving accurate and reliable path following performance and a fixed-time nonlinear estimator is designed for estimating the uncertainties with sideslip angles caused by external disturbances and inertial motions.
Proceedings ArticleDOI

Near minimum-time feedback attitude control with multiple saturation constraints for satellites

TL;DR: In this paper, a near minimum time feedback control law is proposed for the agile satellite attitude control system, which is formed by specially designed cascaded subunits, and the attitude maneuvering can be applied in tasks including the move to move case.
Journal ArticleDOI

State Observer Based Robust Backstepping Fault-Tolerant Control of the Free-Floating Flexible-Joint Space Manipulator

Limin Xie, +1 more
- 17 Feb 2023 - 
TL;DR: In this paper , a state-observer-based robust backstepping fault-tolerant control is proposed for the system joint actuator failure, which can make the free-floating flexible-joint space manipulator system track the desired trajectory accurately and steadily regardless of whether the actuator fails or not.
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

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

Bong Wie
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

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.
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