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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

Global Finite-Time Adaptive Stabilization of Nonlinearly Parametrized Systems With Multiple Unknown Control Directions

TL;DR: A novel logic switching regulation is established based on Lyapunov function method to overcome this main obstacle of the global finite-time adaptive stabilization for nonlinearly parametrized systems with multiple unknown control directions.
Journal ArticleDOI

Fixed-time attitude tracking control for rigid spacecraft

TL;DR: A novel fixed-time attitude control law is proposed based on the backstepping technique and the idea of “adding a power integrator”, and can guarantee the attitude tracking errors converging to the origin within fixed time if there are no uncertainties and measurement noises.
Journal ArticleDOI

Finite-time path following control for a stratospheric airship with input saturation and error constraint

TL;DR: Simulation results illustrate that the proposed finite-time controller offers a faster convergence rate and a higher path following accuracy for the stratospheric airship.
Journal ArticleDOI

Fault-Tolerant Flight Control Design With Finite-Time Adaptation Under Actuator Stuck Failures

TL;DR: An adaptive fault-tolerant flight control (FTFC) scheme to counteract actuator stuck failures, where the issues on saturation avoidance of redundant actuators and finite-time adaptation of FTFC are addressed.
Journal ArticleDOI

Adaptive Finite-Time Attitude Tracking Control for Spacecraft With Disturbances

TL;DR: It is proved that both the two control laws can ensure the tracking errors converge to the desired regions in finite-time and the chattering problem is eliminated.
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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