Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft

Yibo Ding; Yingzi Guan; Naigang Cui; Feng Yang

doi:10.1109/CCDC.2017.7979447

Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft

Yibo Ding
, Yingzi Guan
, Naigang Cui
, Feng Yang

School of Astronautics, Harbin Institute of Technology

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

3 Scopus citations

Abstract

A robust disturbance rejection guidance law for autonomous rendezvous with non-cooperative target is studied using generalized super-twisting algorithm (GSTA) and homogeneous high order sliding mode observer (HHOSMO). The proposed method is able to ensure a service spacecraft subject to modeling uncertainties, external disturbances and actuator/thruster failures accomplishes the rendezvous mission without collision. Considering the restriction of Clohessy-Wiltshire (C-W) equations, a coupled relative motion model is established in line of sight coordinate frame. The GSTA is used as a robust continuous guidance law while the HHOSMO is able to observe and compensate the lumped disturbances in a finite time to enhance the ability of disturbance rejection. The stability of the closed-loop system is analyzed using Lyapunov stability criteria. Results obtained from numerical simulations demonstrate the validity of the method formulated in this paper.

Original language	English
Title of host publication	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5346-5351
Number of pages	6
ISBN (Electronic)	9781509046560
DOIs	https://doi.org/10.1109/CCDC.2017.7979447
State	Published - 12 Jul 2017
Externally published	Yes
Event	29th Chinese Control and Decision Conference, CCDC 2017 - Chongqing, China Duration: 28 May 2017 → 30 May 2017

Publication series

Name	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

Conference

Conference	29th Chinese Control and Decision Conference, CCDC 2017
Country/Territory	China
City	Chongqing
Period	28/05/17 → 30/05/17

Keywords

Disturbance Rejection
Generalized Super-Twisting Algorithm
Homogeneous High
Order Sliding Mode Observer
Rendezvous
Tumbling Non-Cooperative

Access to Document

10.1109/CCDC.2017.7979447

Cite this

Ding, Y., Guan, Y., Cui, N., & Yang, F. (2017). Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017 (pp. 5346-5351). Article 7979447 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2017.7979447

Ding, Yibo ; Guan, Yingzi ; Cui, Naigang et al. / Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft. Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 5346-5351 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

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title = "Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft",

abstract = "A robust disturbance rejection guidance law for autonomous rendezvous with non-cooperative target is studied using generalized super-twisting algorithm (GSTA) and homogeneous high order sliding mode observer (HHOSMO). The proposed method is able to ensure a service spacecraft subject to modeling uncertainties, external disturbances and actuator/thruster failures accomplishes the rendezvous mission without collision. Considering the restriction of Clohessy-Wiltshire (C-W) equations, a coupled relative motion model is established in line of sight coordinate frame. The GSTA is used as a robust continuous guidance law while the HHOSMO is able to observe and compensate the lumped disturbances in a finite time to enhance the ability of disturbance rejection. The stability of the closed-loop system is analyzed using Lyapunov stability criteria. Results obtained from numerical simulations demonstrate the validity of the method formulated in this paper.",

keywords = "Disturbance Rejection, Generalized Super-Twisting Algorithm, Homogeneous High, Order Sliding Mode Observer, Rendezvous, Tumbling Non-Cooperative",

author = "Yibo Ding and Yingzi Guan and Naigang Cui and Feng Yang",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",

year = "2017",

month = jul,

day = "12",

doi = "10.1109/CCDC.2017.7979447",

language = "英语",

series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

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Ding, Y, Guan, Y , Cui, N & Yang, F 2017, Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft. in Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017., 7979447, Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 5346-5351, 29th Chinese Control and Decision Conference, CCDC 2017, Chongqing, China, 28/05/17. https://doi.org/10.1109/CCDC.2017.7979447

Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft. / Ding, Yibo; Guan, Yingzi ; Cui, Naigang et al.
Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 5346-5351 7979447 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

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

TY - GEN

T1 - Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft

AU - Ding, Yibo

AU - Guan, Yingzi

AU - Cui, Naigang

AU - Yang, Feng

PY - 2017/7/12

Y1 - 2017/7/12

N2 - A robust disturbance rejection guidance law for autonomous rendezvous with non-cooperative target is studied using generalized super-twisting algorithm (GSTA) and homogeneous high order sliding mode observer (HHOSMO). The proposed method is able to ensure a service spacecraft subject to modeling uncertainties, external disturbances and actuator/thruster failures accomplishes the rendezvous mission without collision. Considering the restriction of Clohessy-Wiltshire (C-W) equations, a coupled relative motion model is established in line of sight coordinate frame. The GSTA is used as a robust continuous guidance law while the HHOSMO is able to observe and compensate the lumped disturbances in a finite time to enhance the ability of disturbance rejection. The stability of the closed-loop system is analyzed using Lyapunov stability criteria. Results obtained from numerical simulations demonstrate the validity of the method formulated in this paper.

AB - A robust disturbance rejection guidance law for autonomous rendezvous with non-cooperative target is studied using generalized super-twisting algorithm (GSTA) and homogeneous high order sliding mode observer (HHOSMO). The proposed method is able to ensure a service spacecraft subject to modeling uncertainties, external disturbances and actuator/thruster failures accomplishes the rendezvous mission without collision. Considering the restriction of Clohessy-Wiltshire (C-W) equations, a coupled relative motion model is established in line of sight coordinate frame. The GSTA is used as a robust continuous guidance law while the HHOSMO is able to observe and compensate the lumped disturbances in a finite time to enhance the ability of disturbance rejection. The stability of the closed-loop system is analyzed using Lyapunov stability criteria. Results obtained from numerical simulations demonstrate the validity of the method formulated in this paper.

KW - Disturbance Rejection

KW - Generalized Super-Twisting Algorithm

KW - Homogeneous High

KW - Order Sliding Mode Observer

KW - Rendezvous

KW - Tumbling Non-Cooperative

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ER -

Ding Y, Guan Y , Cui N, Yang F. Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 5346-5351. 7979447. (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). doi: 10.1109/CCDC.2017.7979447

Robust disturbance rejection guidance law for autonomous rendezvous with tumbling non-cooperative spacecraft

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