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

Jia Song; Ce Hao; Yanxue Zhang; Nanjia Yu; Yang Liu; Erfu Yang

doi:10.1109/ICCA.2019.8899548

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

Jia Song, Ce Hao, Yanxue Zhang, Nanjia Yu, Yang Liu, Erfu Yang

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

2 Citations (Scopus)

40 Downloads (Pure)

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.

Original language	English
Title of host publication	2019 IEEE 15th International Conference on Control and Automation, ICCA 2019
Place of Publication	Piscataway, N.J.
Publisher	IEEE
Pages	109-114
Number of pages	6
ISBN (Electronic)	9781728111643
DOIs	https://doi.org/10.1109/ICCA.2019.8899548
Publication status	Published - 14 Nov 2019
Event	15th IEEE International Conference on Control and Automation, ICCA 2019 - Edinburgh, United Kingdom Duration: 16 Jul 2019 → 19 Jul 2019

Publication series

Name	IEEE International Conference on Control and Automation, ICCA
Volume	2019-July
ISSN (Print)	1948-3449
ISSN (Electronic)	1948-3457

Conference

Conference	15th IEEE International Conference on Control and Automation, ICCA 2019
Country/Territory	United Kingdom
City	Edinburgh
Period	16/07/19 → 19/07/19

Funding

*This work is supported by Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Minisitry of Education, China.

Keywords

aerodynamics
reentry hypersonic vehicle
trajectory control

Access to Document

10.1109/ICCA.2019.8899548

Song-etal-ICCA-2019-Double-loop-sliding-mode-control-of-reentry-hypersonicAccepted author manuscript, 543 KBLicence: Strath_1

Cite this

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title = "Double-loop sliding mode control of reentry hypersonic vehicle with RCS",

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.",

keywords = "aerodynamics, reentry hypersonic vehicle, trajectory control",

author = "Jia Song and Ce Hao and Yanxue Zhang and Nanjia Yu and Yang Liu and Erfu Yang",

note = "{\textcopyright} 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.; 15th IEEE International Conference on Control and Automation, ICCA 2019 ; Conference date: 16-07-2019 Through 19-07-2019",

year = "2019",

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doi = "10.1109/ICCA.2019.8899548",

language = "English",

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Song, J, Hao, C, Zhang, Y, Yu, N, Liu, Y & Yang, E 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, vol. 2019-July, IEEE, Piscataway, N.J., pp. 109-114, 15th IEEE International Conference on Control and Automation, ICCA 2019, Edinburgh, United Kingdom, 16/07/19. https://doi.org/10.1109/ICCA.2019.8899548

Double-loop sliding mode control of reentry hypersonic vehicle with RCS. / Song, Jia; Hao, Ce; Zhang, Yanxue et al.
2019 IEEE 15th International Conference on Control and Automation, ICCA 2019. Piscataway, N.J.: IEEE, 2019. p. 109-114 (IEEE International Conference on Control and Automation, ICCA; Vol. 2019-July).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution book

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T1 - Double-loop sliding mode control of reentry hypersonic vehicle with RCS

AU - Song, Jia

AU - Hao, Ce

AU - Zhang, Yanxue

AU - Yu, Nanjia

AU - Liu, Yang

AU - Yang, Erfu

N1 - © 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.

PY - 2019/11/14

Y1 - 2019/11/14

N2 - 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.

AB - 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.

KW - aerodynamics

KW - reentry hypersonic vehicle

KW - trajectory control

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PB - IEEE

CY - Piscataway, N.J.

T2 - 15th IEEE International Conference on Control and Automation, ICCA 2019

Y2 - 16 July 2019 through 19 July 2019

ER -

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

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