Compound control system design for RLV based on normalization method

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

doi:10.3873/j.issn.1000-1328.2016.06.002

Compound control system design for RLV based on normalization method

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

School of Astronautics

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

4 Scopus citations

Abstract

A novel compound control system for reusable launch vehicle (RLV) based on normalization method is proposed in the paper. Firstly, a normalization model for RLV including normalized pneumatic model and normalized thrust vector model is built, and a new switching condition for pneumatic/thrust vectoring compound controller by adopting control threshold is derived from the normalization model. Secondly, an integral terminal sliding mode compound controller is designed and assigned control command is accomplished by utilizing the generalized inverse method without optimization algorithm. Finally, the performance and robustness are assessed through a RLV with model parameter perturbations, and the simulation also indicates both the proposed method and the linear programming optimization algorithm can obtain the same performance.

Original language	English
Pages (from-to)	639-645
Number of pages	7
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	37
Issue number	6
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2016.06.002
State	Published - 30 Jun 2016

Keywords

Command allocation
Compound control
Normalization method
Reusable launch vehicle
Terminal sliding mode

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10.3873/j.issn.1000-1328.2016.06.002

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title = "Compound control system design for RLV based on normalization method",

abstract = "A novel compound control system for reusable launch vehicle (RLV) based on normalization method is proposed in the paper. Firstly, a normalization model for RLV including normalized pneumatic model and normalized thrust vector model is built, and a new switching condition for pneumatic/thrust vectoring compound controller by adopting control threshold is derived from the normalization model. Secondly, an integral terminal sliding mode compound controller is designed and assigned control command is accomplished by utilizing the generalized inverse method without optimization algorithm. Finally, the performance and robustness are assessed through a RLV with model parameter perturbations, and the simulation also indicates both the proposed method and the linear programming optimization algorithm can obtain the same performance.",

keywords = "Command allocation, Compound control, Normalization method, Reusable launch vehicle, Terminal sliding mode",

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

year = "2016",

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doi = "10.3873/j.issn.1000-1328.2016.06.002",

language = "英语",

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TY - JOUR

T1 - Compound control system design for RLV based on normalization method

AU - Guo, Jian Guo

AU - Zhang, Tian Bao

AU - Zhou, Jun

AU - Wang, Guo Qing

AU - Zhang, Yue Ling

PY - 2016/6/30

Y1 - 2016/6/30

N2 - A novel compound control system for reusable launch vehicle (RLV) based on normalization method is proposed in the paper. Firstly, a normalization model for RLV including normalized pneumatic model and normalized thrust vector model is built, and a new switching condition for pneumatic/thrust vectoring compound controller by adopting control threshold is derived from the normalization model. Secondly, an integral terminal sliding mode compound controller is designed and assigned control command is accomplished by utilizing the generalized inverse method without optimization algorithm. Finally, the performance and robustness are assessed through a RLV with model parameter perturbations, and the simulation also indicates both the proposed method and the linear programming optimization algorithm can obtain the same performance.

AB - A novel compound control system for reusable launch vehicle (RLV) based on normalization method is proposed in the paper. Firstly, a normalization model for RLV including normalized pneumatic model and normalized thrust vector model is built, and a new switching condition for pneumatic/thrust vectoring compound controller by adopting control threshold is derived from the normalization model. Secondly, an integral terminal sliding mode compound controller is designed and assigned control command is accomplished by utilizing the generalized inverse method without optimization algorithm. Finally, the performance and robustness are assessed through a RLV with model parameter perturbations, and the simulation also indicates both the proposed method and the linear programming optimization algorithm can obtain the same performance.

KW - Command allocation

KW - Compound control

KW - Normalization method

KW - Reusable launch vehicle

KW - Terminal sliding mode

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DO - 10.3873/j.issn.1000-1328.2016.06.002

M3 - 文章

AN - SCOPUS:84977472183

SN - 1000-1328

VL - 37

SP - 639

EP - 645

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 6

ER -

Compound control system design for RLV based on normalization method

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Keywords

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