Double-loop sliding mode control of reentry hypersonic vehicle with RCS

Song, Jia and Hao, Ce and Zhang, Yanxue and Yu, Nanjia and Liu, Yang and Yang, Erfu; (2019) Double-loop sliding mode control of reentry hypersonic vehicle with RCS. In: 2019 IEEE 15th International Conference on Control and Automation, ICCA 2019. IEEE International Conference on Control and Automation, ICCA . IEEE, GBR, pp. 109-114. ISBN 9781728111643

[img]
Preview
 Text (Song-etal-ICCA-2019-Double-loop-sliding-mode-control-of-reentry-hypersonic)
Song_etal_ICCA_2019_Double_loop_sliding_mode_control_of_reentry_hypersonic.pdf
Accepted Author Manuscript
Download (555kB)| Preview

    Abstract

    In order to solve the problem of insufficient aerodynamic moment caused by thin air in the re-entry stage of hypersonic vehicle, this paper establishes an attitude angle model of hypersonic vehicle with reaction control system (RCS), and derives its affine linear model to decoupled the internal and external loop. According to the dead zone and saturation characteristics of RCS thruster, a control method to convert continuous moment into discrete switching instruction using pulse width modulation (PWM) is proposed. Since the number of thrusters is usually redundant, the installation matrix of thrusters in the body coordinate is established, and the command moment is coordinately distributed to the individual thrusters. Then a double-loop sliding mode controller (DSMC) is designed to achieve attitude stability and trajectory tracking. Finally, the simulation results show that DSMC has higher maneuverability, fewer thruster switches and stronger robustness to interference.

    Creators(s): Song, Jia, Hao, Ce, Zhang, Yanxue, Yu, Nanjia, Liu, Yang and Yang, Erfu ORCID logoORCID: https://orcid.org/0000-0003-1813-5950;
    Item type:Book Section
    ID code:72116
    Notes:© 2019 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting /republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.
    Keywords:aerodynamics, reentry hypersonic vehicle, trajectory control, Motor vehicles. Aeronautics. Astronautics, Artificial Intelligence, Computer Science Applications, Control and Systems Engineering, Electrical and Electronic Engineering, Industrial and Manufacturing Engineering
    Subjects:Technology > Motor vehicles. Aeronautics. Astronautics
    Department:Faculty of Engineering > Design, Manufacture and Engineering Management
    Faculty of Humanities and Social Sciences (HaSS) > School of Psychological Science and Health
    Depositing user: Pure Administrator
    Date deposited:21 Apr 2020 10:49
    Last modified:15 Sep 2020 08:49
    Related URLs:
    URI:https://strathprints.strath.ac.uk/id/eprint/72116
    Export data:
    CORE (COnnecting REpositories)