Velocity-Free Guidance Scheme for Close-Range Rendezvous

Xingwei Shi; Wei Wang; Defu Lin; Yi Ji

doi:10.1109/GNCC42960.2018.9019050

Velocity-Free Guidance Scheme for Close-Range Rendezvous

Xingwei Shi, Wei Wang, Defu Lin, Yi Ji

School of Aerospace Engineering

Beijing Institute of Technology

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

Abstract

A novel multiple-input-multiple-output(MIMO) guidance scheme is proposed for reliable spacecraft rendezvous in the presence of external uncertain disturbance in this paper. To estimate the unknown relative velocity between the chaser and the target in real time, a novel finite-time convergent observer based on second-order sliding mode theory is proposed. Next, a MIMO guidance scheme based on super-twisting control theory is proposed to drive the relative range and its rate converge to a small compact region around zero in finite time. The stability of the closed-loop system is verified via Lyapunov theory. The results of numerical simulation demonstrate the effectiveness of the proposed guidance scheme.

Original language	English
Title of host publication	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)	9781538611715
DOIs	https://doi.org/10.1109/GNCC42960.2018.9019050
Publication status	Published - Aug 2018
Event	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, China Duration: 10 Aug 2018 → 12 Aug 2018

Publication series

Name	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Conference

Conference	2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Country/Territory	China
City	Xiamen
Period	10/08/18 → 12/08/18

Keywords

Spacecraft rendezvous
finite-time convergence
multivariable sliding mode
velocity-free.

Access to Document

10.1109/GNCC42960.2018.9019050

Cite this

@inproceedings{6c9da21912be4f31aff0ccc2d03eb981,

title = "Velocity-Free Guidance Scheme for Close-Range Rendezvous",

abstract = "A novel multiple-input-multiple-output(MIMO) guidance scheme is proposed for reliable spacecraft rendezvous in the presence of external uncertain disturbance in this paper. To estimate the unknown relative velocity between the chaser and the target in real time, a novel finite-time convergent observer based on second-order sliding mode theory is proposed. Next, a MIMO guidance scheme based on super-twisting control theory is proposed to drive the relative range and its rate converge to a small compact region around zero in finite time. The stability of the closed-loop system is verified via Lyapunov theory. The results of numerical simulation demonstrate the effectiveness of the proposed guidance scheme.",

keywords = "Spacecraft rendezvous, finite-time convergence, multivariable sliding mode, velocity-free.",

author = "Xingwei Shi and Wei Wang and Defu Lin and Yi Ji",

note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 ; Conference date: 10-08-2018 Through 12-08-2018",

year = "2018",

month = aug,

doi = "10.1109/GNCC42960.2018.9019050",

language = "English",

series = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",

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

booktitle = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",

address = "United States",

}

Shi, X, Wang, W , Lin, D & Ji, Y 2018, Velocity-Free Guidance Scheme for Close-Range Rendezvous. in 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018., 9019050, 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018, Institute of Electrical and Electronics Engineers Inc., 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018, Xiamen, China, 10/08/18. https://doi.org/10.1109/GNCC42960.2018.9019050

Velocity-Free Guidance Scheme for Close-Range Rendezvous. / Shi, Xingwei; Wang, Wei ; Lin, Defu et al.
2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018. Institute of Electrical and Electronics Engineers Inc., 2018. 9019050 (2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018).

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

TY - GEN

T1 - Velocity-Free Guidance Scheme for Close-Range Rendezvous

AU - Shi, Xingwei

AU - Wang, Wei

AU - Lin, Defu

AU - Ji, Yi

PY - 2018/8

Y1 - 2018/8

N2 - A novel multiple-input-multiple-output(MIMO) guidance scheme is proposed for reliable spacecraft rendezvous in the presence of external uncertain disturbance in this paper. To estimate the unknown relative velocity between the chaser and the target in real time, a novel finite-time convergent observer based on second-order sliding mode theory is proposed. Next, a MIMO guidance scheme based on super-twisting control theory is proposed to drive the relative range and its rate converge to a small compact region around zero in finite time. The stability of the closed-loop system is verified via Lyapunov theory. The results of numerical simulation demonstrate the effectiveness of the proposed guidance scheme.

AB - A novel multiple-input-multiple-output(MIMO) guidance scheme is proposed for reliable spacecraft rendezvous in the presence of external uncertain disturbance in this paper. To estimate the unknown relative velocity between the chaser and the target in real time, a novel finite-time convergent observer based on second-order sliding mode theory is proposed. Next, a MIMO guidance scheme based on super-twisting control theory is proposed to drive the relative range and its rate converge to a small compact region around zero in finite time. The stability of the closed-loop system is verified via Lyapunov theory. The results of numerical simulation demonstrate the effectiveness of the proposed guidance scheme.

KW - Spacecraft rendezvous

KW - finite-time convergence

KW - multivariable sliding mode

KW - velocity-free.

UR - http://www.scopus.com/inward/record.url?scp=85082464390&partnerID=8YFLogxK

U2 - 10.1109/GNCC42960.2018.9019050

DO - 10.1109/GNCC42960.2018.9019050

M3 - Conference contribution

AN - SCOPUS:85082464390

T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

Y2 - 10 August 2018 through 12 August 2018

ER -

Velocity-Free Guidance Scheme for Close-Range Rendezvous

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Keywords

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