Prescribed Performance Attitude Stabilization of a Rigid Body under Physical Limitations

Journal article


Authors/Editors


Strategic Research Themes


Publication Details

Author listGolestani, Mehdi; Mobayen, Saleh; Din, Sami Ud; El-Sousy, Fayez F. M.; Vu, Mai The; Assawinchaichote, Wudhichai;

PublisherInstitute of Electrical and Electronics Engineers

Publication year2022

Volume number58

Issue number5

Start page4147

End page4155

Number of pages9

ISSN0018-9251

eISSN1557-9603

URLhttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85127059240&doi=10.1109%2fTAES.2022.3158371&partnerID=40&md5=e26336b7be8fa882f2ca2bebcf0c1b35

LanguagesEnglish-Great Britain (EN-GB)


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Abstract

This article investigates the prescribed performance control problem associated with attitude stabilization of a rigid body, considering angular velocity constraint, actuator faults, and input saturation. The desired performance specifications in transient and steady-state phases including convergence speed, overshoot, and steady-state value for attitude variable are also provided. To this end, the prescribed performance control methodology is combined with backstepping-based barrier Lyapunov function so as to develop a controller with simple structure compared to the existing constrained controls. The main idea behind the control design is to remove partial differential and complex function terms to considerably decrease complexity of the proposed controller. Moreover, a hyperbolic tangent function and an auxiliary system are employed to develop the constrained virtual rotation velocity control and to consider input saturation. The simulation results carried out on a rigid spacecraft confirm efficiency and success of the proposed constrained attitude control method. © 1965-2011 IEEE.


Keywords

Angular velocity constraintattitude controlbarrier Lyapunov function (BLF)prescribed performance control (PPC)


Last updated on 2023-03-10 at 07:37