Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint

Binglong Cong; Xiangdong Liu; Zhen Chen; Xianren Ren

doi:10.1109/CCDC.2011.5968267

Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint

Binglong Cong^*, Xiangdong Liu, Zhen Chen, Xianren Ren

^*Corresponding author for this work

School of Automation

Beijing Institute of Technology

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

9 Citations (Scopus)

Abstract

In this paper, the attitude control problem for uncertain spacecraft under angular velocity constraint is addressed. Both parametric uncertainty and external disturbance are considered in the spacecraft's dynamics. The spacecraft's attitude is represented by modified Rodrigues parameter (MRP) for its non-redundancy. A time-varying sliding mode control (TVSMC) algorithm is derived for attitude control system. The proposed control algorithm eliminates the reaching phase of the conventional time-invariant sliding mode control (SMC) and guarantees the sliding mode occurrence all the time. Moreover, the control parameter is adjusted to avoid the angular velocity constraint during the maneuver. Finally, a numerical simulation is employed to verify the proposed control algorithm.

Original language	English
Title of host publication	Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011
Pages	670-674
Number of pages	5
DOIs	https://doi.org/10.1109/CCDC.2011.5968267
Publication status	Published - 2011
Event	2011 Chinese Control and Decision Conference, CCDC 2011 - Mianyang, China Duration: 23 May 2011 → 25 May 2011

Publication series

Name	Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

Conference

Conference	2011 Chinese Control and Decision Conference, CCDC 2011
Country/Territory	China
City	Mianyang
Period	23/05/11 → 25/05/11

Keywords

Angular Velocity Constraint
Attitude Maneuver
Time-varying Sliding Mode Control
Uncertain Spacecraft

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10.1109/CCDC.2011.5968267

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Cong, B., Liu, X., Chen, Z., & Ren, X. (2011). Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint. In Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011 (pp. 670-674). Article 5968267 (Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011). https://doi.org/10.1109/CCDC.2011.5968267

@inproceedings{00cd9bddf61746a2a48ffa4a1fed1277,

title = "Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint",

abstract = "In this paper, the attitude control problem for uncertain spacecraft under angular velocity constraint is addressed. Both parametric uncertainty and external disturbance are considered in the spacecraft's dynamics. The spacecraft's attitude is represented by modified Rodrigues parameter (MRP) for its non-redundancy. A time-varying sliding mode control (TVSMC) algorithm is derived for attitude control system. The proposed control algorithm eliminates the reaching phase of the conventional time-invariant sliding mode control (SMC) and guarantees the sliding mode occurrence all the time. Moreover, the control parameter is adjusted to avoid the angular velocity constraint during the maneuver. Finally, a numerical simulation is employed to verify the proposed control algorithm.",

keywords = "Angular Velocity Constraint, Attitude Maneuver, Time-varying Sliding Mode Control, Uncertain Spacecraft",

author = "Binglong Cong and Xiangdong Liu and Zhen Chen and Xianren Ren",

year = "2011",

doi = "10.1109/CCDC.2011.5968267",

language = "English",

isbn = "9781424487363",

series = "Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011",

pages = "670--674",

booktitle = "Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011",

note = "2011 Chinese Control and Decision Conference, CCDC 2011 ; Conference date: 23-05-2011 Through 25-05-2011",

}

Cong, B, Liu, X , Chen, Z & Ren, X 2011, Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint. in Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011., 5968267, Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011, pp. 670-674, 2011 Chinese Control and Decision Conference, CCDC 2011, Mianyang, China, 23/05/11. https://doi.org/10.1109/CCDC.2011.5968267

Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint. / Cong, Binglong; Liu, Xiangdong ; Chen, Zhen et al.
Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011. 2011. p. 670-674 5968267 (Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011).

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

TY - GEN

T1 - Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint

AU - Cong, Binglong

AU - Liu, Xiangdong

AU - Chen, Zhen

AU - Ren, Xianren

PY - 2011

Y1 - 2011

N2 - In this paper, the attitude control problem for uncertain spacecraft under angular velocity constraint is addressed. Both parametric uncertainty and external disturbance are considered in the spacecraft's dynamics. The spacecraft's attitude is represented by modified Rodrigues parameter (MRP) for its non-redundancy. A time-varying sliding mode control (TVSMC) algorithm is derived for attitude control system. The proposed control algorithm eliminates the reaching phase of the conventional time-invariant sliding mode control (SMC) and guarantees the sliding mode occurrence all the time. Moreover, the control parameter is adjusted to avoid the angular velocity constraint during the maneuver. Finally, a numerical simulation is employed to verify the proposed control algorithm.

AB - In this paper, the attitude control problem for uncertain spacecraft under angular velocity constraint is addressed. Both parametric uncertainty and external disturbance are considered in the spacecraft's dynamics. The spacecraft's attitude is represented by modified Rodrigues parameter (MRP) for its non-redundancy. A time-varying sliding mode control (TVSMC) algorithm is derived for attitude control system. The proposed control algorithm eliminates the reaching phase of the conventional time-invariant sliding mode control (SMC) and guarantees the sliding mode occurrence all the time. Moreover, the control parameter is adjusted to avoid the angular velocity constraint during the maneuver. Finally, a numerical simulation is employed to verify the proposed control algorithm.

KW - Angular Velocity Constraint

KW - Attitude Maneuver

KW - Time-varying Sliding Mode Control

KW - Uncertain Spacecraft

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U2 - 10.1109/CCDC.2011.5968267

DO - 10.1109/CCDC.2011.5968267

M3 - Conference contribution

AN - SCOPUS:80052247678

SN - 9781424487363

T3 - Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

SP - 670

EP - 674

BT - Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011

T2 - 2011 Chinese Control and Decision Conference, CCDC 2011

Y2 - 23 May 2011 through 25 May 2011

ER -

Time-varying sliding mode control for spacecraft attitude maneuver with angular velocity constraint

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