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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

Attitude tracking control of spacecraft with preset‐time preset‐bounded convergence

TL;DR: In this paper , a nonsingular and continuous preset-time preset-bounded attitude tracking control scheme is developed for rigid spacecraft in the presence of bounded external disturbances, which exhibits superiority in reducing the magnitude of the applied control torques and saving energy.
Journal ArticleDOI

Finite Time Adaptive Neural Dynamic Surface Control of Nonstrict Feedback Nonlinear Systems Including Dead-Zone and Full State Restrictions

TL;DR: Through finite-time stability theory and introducing the bounded closed set in the proof, all the signals in the closed-loop system are proved to be semi-globally practical finite time stable (SGPFS).
Proceedings ArticleDOI

Adaptive Fuzzy Finite-time Tracking Control for A Class of DC Motor with State Constraints

TL;DR: In this paper, an adaptive fuzzy finite-time control scheme for a class of direct-current (DC) motor with state constraints is presented, where the barrier Lyapunov function is used to constrain the state variables of the motor to ensure that the angular position and angular velocity of the DC motor are limited within the given constraint range.
Journal ArticleDOI

Fixed time output feedback control for quadrotor unmanned aerial vehicle under disturbances

TL;DR: In this paper , a fixed time output feedback trajectory tracking control scheme for quadrotor Unmanned Aerial Vehicle with unmeasurable velocity and external disturbances is proposed. But the proposed scheme is not suitable for UAVs.
Journal ArticleDOI

Adaptive Control strategy based reference model for Spacecraft Motion Trajectory

TL;DR: In this article, a viable adaptive control approach (ACA) for Spacecraft Motion Trajectory (SMT) is proposed, which involves the nonlinear mathematical model of SMT expressed in the central field, which is linearized by the Taylor expansion, and the second Lyapunov method.
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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