Reaction control system design for reentry vehicle

Jian Guo Guo; Tian Bao Zhang; Jun Zhou; Guo Qing Wang

doi:10.7673/j.issn.1006-2793.2017.04.020

Reaction control system design for reentry vehicle

Jian Guo Guo
, Tian Bao Zhang
, Jun Zhou
, Guo Qing Wang

School of Astronautics

Northwestern Polytechnical University Xian
China Aerospace Science and Technology Corporation

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

According to the tracking error of reaction control system (RCS), a new precision control strategy is proposed for the initial reentry phase of reentry vehicle. Firstly, a nonlinear disturbance observer (DOB) is used for observing the model uncertainty and/or external disturbances. Secondly, a sliding mode control system for the fast loop and slow loop is designed by back-stepping style, and obtained the optimal combination of RCS by linear optimization. Besides, a Integral PWPF Modulator (IPWPF) is proposed based on traditional PWPF modulator, and its stability is proved by a describing function. Finally, the simulation indicates a great precision of the method.

Original language	English
Pages (from-to)	511-516
Number of pages	6
Journal	Guti Huojian Jishu/Journal of Solid Rocket Technology
Volume	40
Issue number	4
DOIs	https://doi.org/10.7673/j.issn.1006-2793.2017.04.020
State	Published - 1 Aug 2017

Keywords

Disturbance observer
PWPF modulator
Reaction control system
Reentry vehicle
Sliding mode

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10.7673/j.issn.1006-2793.2017.04.020

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title = "Reaction control system design for reentry vehicle",

abstract = "According to the tracking error of reaction control system (RCS), a new precision control strategy is proposed for the initial reentry phase of reentry vehicle. Firstly, a nonlinear disturbance observer (DOB) is used for observing the model uncertainty and/or external disturbances. Secondly, a sliding mode control system for the fast loop and slow loop is designed by back-stepping style, and obtained the optimal combination of RCS by linear optimization. Besides, a Integral PWPF Modulator (IPWPF) is proposed based on traditional PWPF modulator, and its stability is proved by a describing function. Finally, the simulation indicates a great precision of the method.",

keywords = "Disturbance observer, PWPF modulator, Reaction control system, Reentry vehicle, Sliding mode",

author = "Guo, \{Jian Guo\} and Zhang, \{Tian Bao\} and Jun Zhou and Wang, \{Guo Qing\}",

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TY - JOUR

T1 - Reaction control system design for reentry vehicle

AU - Guo, Jian Guo

AU - Zhang, Tian Bao

AU - Zhou, Jun

AU - Wang, Guo Qing

PY - 2017/8/1

Y1 - 2017/8/1

N2 - According to the tracking error of reaction control system (RCS), a new precision control strategy is proposed for the initial reentry phase of reentry vehicle. Firstly, a nonlinear disturbance observer (DOB) is used for observing the model uncertainty and/or external disturbances. Secondly, a sliding mode control system for the fast loop and slow loop is designed by back-stepping style, and obtained the optimal combination of RCS by linear optimization. Besides, a Integral PWPF Modulator (IPWPF) is proposed based on traditional PWPF modulator, and its stability is proved by a describing function. Finally, the simulation indicates a great precision of the method.

AB - According to the tracking error of reaction control system (RCS), a new precision control strategy is proposed for the initial reentry phase of reentry vehicle. Firstly, a nonlinear disturbance observer (DOB) is used for observing the model uncertainty and/or external disturbances. Secondly, a sliding mode control system for the fast loop and slow loop is designed by back-stepping style, and obtained the optimal combination of RCS by linear optimization. Besides, a Integral PWPF Modulator (IPWPF) is proposed based on traditional PWPF modulator, and its stability is proved by a describing function. Finally, the simulation indicates a great precision of the method.

KW - Disturbance observer

KW - PWPF modulator

KW - Reaction control system

KW - Reentry vehicle

KW - Sliding mode

UR - https://www.scopus.com/pages/publications/85029827779

U2 - 10.7673/j.issn.1006-2793.2017.04.020

DO - 10.7673/j.issn.1006-2793.2017.04.020

M3 - 文章

AN - SCOPUS:85029827779

SN - 1006-2793

VL - 40

SP - 511

EP - 516

JO - Guti Huojian Jishu/Journal of Solid Rocket Technology

JF - Guti Huojian Jishu/Journal of Solid Rocket Technology

IS - 4

ER -

Reaction control system design for reentry vehicle

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