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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

Neural-Network-Based Adaptive Tracking Control for Nonlinear Multiagent Systems: The Observer Case

TL;DR: In this paper , a neural-network-based adaptive tracking control scheme was proposed for a class of high-order nonlinear multiagent systems both subjected to the immeasurable state variables and unknown external disturbance.
Journal ArticleDOI

Fault‐tolerant attitude tracking control with practical finite time convergence for unmanned aerial vehicles under actuation faults

TL;DR: In this article , an adaptive attitude finite time tracking control algorithm for quadrotor unmanned aerial vehicle (UAV) in presence of actuator faults, input saturation and external disturbance is presented.

Model-Less Fuzzy Logic Control for the NASA Modeling and Control for Agile Aircraft Development Program

TL;DR: The design of a fuzzy PID controller, governed by a fuzzy supervisory system which incorporates knowledge of first principles of flight, to control a model-less aircraft’s pitch dynamics in a free-to-pitch wind-tunnel environment is presented.
Journal ArticleDOI

Finite-Time Attitude Tracking Control of Spacecraft with Actuator Saturation

TL;DR: The attitude tracking control problem of a rigid spacecraft with actuator saturation is investigated by incorporating sliding mode control (SMC) and adaptive technique and it is shown that attitude tracking error can converge to zero in a finite time with the aid of the developed sliding dynamics.
Proceedings ArticleDOI

Analysis of Nonlinearity and Dynamic Coupling in Fast Circumnavigation Missions

TL;DR: The non-linear dynamics and linear dynamics of the fast circumnavigation mission are established and show that the non- linear characteristics of attitude dynamics seriously affect the control quality of relative orbit position, which means that the linear model is not suitable for situations that require synchronous and high-precision control of attitude and orbit.
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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