Underactuated spacecraft chaotic attitude control based on exponential reaching law

Zhaowei Sun; Chuang Liu; Keke Shi; Jianqiao Zhang

doi:10.1109/ICMAE.2017.8038718

Underactuated spacecraft chaotic attitude control based on exponential reaching law

Zhaowei Sun
, Chuang Liu
, Keke Shi
, Jianqiao Zhang

School of Astronautics

Harbin Institute of Technology

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

2 Scopus citations

Abstract

The control problem of underactuated spacecraft chaotic attitude motion is investigated based on exponential reaching law in this paper. First, the underactuated spacecraft chaotic attitude system is written in nonlinear equation form with two controls. Once the trajectory planning of angular acceleration is preset, the dynamics equation of angular velocity error can be obtained. Then, the sliding mode controller based on exponential reaching law and linear matrix inequality is designed, which consists of equivalent control term and switching control term. Finally, simulations are performed to test the performance of the proposed controller.

Original language	English
Title of host publication	2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	615-619
Number of pages	5
ISBN (Electronic)	9781538633052
DOIs	https://doi.org/10.1109/ICMAE.2017.8038718
State	Published - 14 Sep 2017
Event	8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 - Prague, Czech Republic Duration: 22 Jul 2017 → 25 Jul 2017

Publication series

Name	2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

Conference

Conference	8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
Country/Territory	Czech Republic
City	Prague
Period	22/07/17 → 25/07/17

Keywords

attitude system
chaotic motion
exponential reaching law
linear matrix inequality
underactuated spacecraft

Access to Document

10.1109/ICMAE.2017.8038718

Cite this

Sun, Z., Liu, C., Shi, K., & Zhang, J. (2017). Underactuated spacecraft chaotic attitude control based on exponential reaching law. In 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 (pp. 615-619). Article 8038718 (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMAE.2017.8038718

Sun, Zhaowei ; Liu, Chuang ; Shi, Keke et al. / Underactuated spacecraft chaotic attitude control based on exponential reaching law. 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 615-619 (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017).

@inproceedings{cfc14b8c861d4e5ba9312dfb1150e449,

title = "Underactuated spacecraft chaotic attitude control based on exponential reaching law",

abstract = "The control problem of underactuated spacecraft chaotic attitude motion is investigated based on exponential reaching law in this paper. First, the underactuated spacecraft chaotic attitude system is written in nonlinear equation form with two controls. Once the trajectory planning of angular acceleration is preset, the dynamics equation of angular velocity error can be obtained. Then, the sliding mode controller based on exponential reaching law and linear matrix inequality is designed, which consists of equivalent control term and switching control term. Finally, simulations are performed to test the performance of the proposed controller.",

keywords = "attitude system, chaotic motion, exponential reaching law, linear matrix inequality, underactuated spacecraft",

author = "Zhaowei Sun and Chuang Liu and Keke Shi and Jianqiao Zhang",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 ; Conference date: 22-07-2017 Through 25-07-2017",

year = "2017",

month = sep,

day = "14",

doi = "10.1109/ICMAE.2017.8038718",

language = "英语",

series = "2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

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booktitle = "2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017",

address = "美国",

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Sun, Z, Liu, C, Shi, K & Zhang, J 2017, Underactuated spacecraft chaotic attitude control based on exponential reaching law. in 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017., 8038718, 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017, Institute of Electrical and Electronics Engineers Inc., pp. 615-619, 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017, Prague, Czech Republic, 22/07/17. https://doi.org/10.1109/ICMAE.2017.8038718

Underactuated spacecraft chaotic attitude control based on exponential reaching law. / Sun, Zhaowei; Liu, Chuang; Shi, Keke et al.
2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 615-619 8038718 (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017).

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

TY - GEN

T1 - Underactuated spacecraft chaotic attitude control based on exponential reaching law

AU - Sun, Zhaowei

AU - Liu, Chuang

AU - Shi, Keke

AU - Zhang, Jianqiao

PY - 2017/9/14

Y1 - 2017/9/14

N2 - The control problem of underactuated spacecraft chaotic attitude motion is investigated based on exponential reaching law in this paper. First, the underactuated spacecraft chaotic attitude system is written in nonlinear equation form with two controls. Once the trajectory planning of angular acceleration is preset, the dynamics equation of angular velocity error can be obtained. Then, the sliding mode controller based on exponential reaching law and linear matrix inequality is designed, which consists of equivalent control term and switching control term. Finally, simulations are performed to test the performance of the proposed controller.

AB - The control problem of underactuated spacecraft chaotic attitude motion is investigated based on exponential reaching law in this paper. First, the underactuated spacecraft chaotic attitude system is written in nonlinear equation form with two controls. Once the trajectory planning of angular acceleration is preset, the dynamics equation of angular velocity error can be obtained. Then, the sliding mode controller based on exponential reaching law and linear matrix inequality is designed, which consists of equivalent control term and switching control term. Finally, simulations are performed to test the performance of the proposed controller.

KW - attitude system

KW - chaotic motion

KW - exponential reaching law

KW - linear matrix inequality

KW - underactuated spacecraft

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U2 - 10.1109/ICMAE.2017.8038718

DO - 10.1109/ICMAE.2017.8038718

M3 - 会议稿件

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BT - 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

Y2 - 22 July 2017 through 25 July 2017

ER -

Sun Z, Liu C, Shi K, Zhang J. Underactuated spacecraft chaotic attitude control based on exponential reaching law. In 2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 615-619. 8038718. (2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017). doi: 10.1109/ICMAE.2017.8038718

Underactuated spacecraft chaotic attitude control based on exponential reaching law

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