MPC-based design of on-off control law of the attitude control thruster

Baoqing Yang; Fenghua He; Yu Yao

doi:10.1109/CHICC.2008.4605311

MPC-based design of on-off control law of the attitude control thruster

Baoqing Yang^*
, Fenghua He
, Yu Yao

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

4 Scopus citations

Abstract

The problem of attitude control of exo-atmospheric aerocraft with thruster is researched in this paper. According to the characters of on-off control, multiple step design procedure is proposed. Based on model predictive control theory, a constrained robust attitude control law is designed, and then the on-off control law is obtained via output equivalent. To cope with the limit of minimum pulse width, an improved control law is presented. The proposed method is applied to control of rolling channel, simulation results showed that this control law met the requirements of precision even though disturbance moment reached ten percent of maximum moment, which proved the effectiveness of the proposed method farther.

Original language	English
Title of host publication	Proceedings of the 27th Chinese Control Conference, CCC
Pages	539-543
Number of pages	5
DOIs	https://doi.org/10.1109/CHICC.2008.4605311
State	Published - 2008
Event	27th Chinese Control Conference, CCC - Kunming, Yunnan, China Duration: 16 Jul 2008 → 18 Jul 2008

Publication series

Name	Proceedings of the 27th Chinese Control Conference, CCC

Conference

Conference	27th Chinese Control Conference, CCC
Country/Territory	China
City	Kunming, Yunnan
Period	16/07/08 → 18/07/08

Keywords

Attitude control
Control constrained
Model predictive control

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10.1109/CHICC.2008.4605311

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title = "MPC-based design of on-off control law of the attitude control thruster",

abstract = "The problem of attitude control of exo-atmospheric aerocraft with thruster is researched in this paper. According to the characters of on-off control, multiple step design procedure is proposed. Based on model predictive control theory, a constrained robust attitude control law is designed, and then the on-off control law is obtained via output equivalent. To cope with the limit of minimum pulse width, an improved control law is presented. The proposed method is applied to control of rolling channel, simulation results showed that this control law met the requirements of precision even though disturbance moment reached ten percent of maximum moment, which proved the effectiveness of the proposed method farther.",

keywords = "Attitude control, Control constrained, Model predictive control",

author = "Baoqing Yang and Fenghua He and Yu Yao",

year = "2008",

doi = "10.1109/CHICC.2008.4605311",

language = "英语",

isbn = "9787900719706",

series = "Proceedings of the 27th Chinese Control Conference, CCC",

pages = "539--543",

booktitle = "Proceedings of the 27th Chinese Control Conference, CCC",

note = "27th Chinese Control Conference, CCC ; Conference date: 16-07-2008 Through 18-07-2008",

}

TY - GEN

T1 - MPC-based design of on-off control law of the attitude control thruster

AU - Yang, Baoqing

AU - He, Fenghua

AU - Yao, Yu

PY - 2008

Y1 - 2008

N2 - The problem of attitude control of exo-atmospheric aerocraft with thruster is researched in this paper. According to the characters of on-off control, multiple step design procedure is proposed. Based on model predictive control theory, a constrained robust attitude control law is designed, and then the on-off control law is obtained via output equivalent. To cope with the limit of minimum pulse width, an improved control law is presented. The proposed method is applied to control of rolling channel, simulation results showed that this control law met the requirements of precision even though disturbance moment reached ten percent of maximum moment, which proved the effectiveness of the proposed method farther.

AB - The problem of attitude control of exo-atmospheric aerocraft with thruster is researched in this paper. According to the characters of on-off control, multiple step design procedure is proposed. Based on model predictive control theory, a constrained robust attitude control law is designed, and then the on-off control law is obtained via output equivalent. To cope with the limit of minimum pulse width, an improved control law is presented. The proposed method is applied to control of rolling channel, simulation results showed that this control law met the requirements of precision even though disturbance moment reached ten percent of maximum moment, which proved the effectiveness of the proposed method farther.

KW - Attitude control

KW - Control constrained

KW - Model predictive control

UR - https://www.scopus.com/pages/publications/52649161809

U2 - 10.1109/CHICC.2008.4605311

DO - 10.1109/CHICC.2008.4605311

M3 - 会议稿件

AN - SCOPUS:52649161809

SN - 9787900719706

T3 - Proceedings of the 27th Chinese Control Conference, CCC

SP - 539

EP - 543

BT - Proceedings of the 27th Chinese Control Conference, CCC

T2 - 27th Chinese Control Conference, CCC

Y2 - 16 July 2008 through 18 July 2008

ER -

MPC-based design of on-off control law of the attitude control thruster

Abstract

Publication series

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Keywords

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