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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

Fixed-Time-Synchronized Consensus Control of Multiagent Systems

TL;DR: A singularity-free sliding mode control law is designed to solve the fixed-time-synchronized consensus problem and is presented as a special kind of fixed/finite-time stability, where all the elements of the system state synchronously arrive at the equilibrium at the same time.
Journal ArticleDOI

Adaptive super-twisting nonsingular fast terminal sliding mode control for cable-driven manipulators using time-delay estimation

TL;DR: The validity and superiorities of the newly proposed TDE-based AST-NFTSM control scheme were demonstrated through comparative 2-DOFs (degree of freedoms) simulation and experiments.
Journal ArticleDOI

Adaptive finite-time attitude stabilization for rigid spacecraft with actuator faults and saturation constraints

TL;DR: In this article, a fast terminal sliding mode manifold is designed to avoid the singularity problem while providing high control ability, and a practical adaptive fast-terminal sliding mode control law is presented to guarantee attitude stabilization in finite time.
Journal ArticleDOI

Terminal Sliding Mode-Based Consensus Tracking Control for Networked Uncertain Mechanical Systems on Digraphs

TL;DR: This brief investigates the finite-time consensus tracking control problem for networked uncertain mechanical systems on digraphs and develops a new terminal sliding-mode-based cooperative control scheme to guarantee that the tracking errors converge to an arbitrarily small bound around zero in finite time.
Journal ArticleDOI

Robust terminal angle constraint guidance law with autopilot lag for intercepting maneuvering targets

TL;DR: In this article, a robust continuous guidance law with terminal angle constraint for intercepting maneuvering targets in the presence of autopilot lag is proposed and its finite-time stability is proved.
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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