A super-twisting sliding mode control in a backstepping setup for rendezvous with a passive target

Jazmín Zenteno Torres; Jérôme Cieslak; David Henry; Jorge Dávila

doi:10.1016/j.ifacol.2019.11.064

A super-twisting sliding mode control in a backstepping setup for rendezvous with a passive target

Jazmín Zenteno Torres, Jérôme Cieslak, David Henry, Jorge Dávila

Escuela Superior de Ingeniería Mecánica y Eléctrica (ESIME), Unidad Ticomán

Research output: Contribution to journal › Conference article › peer-review

6 Scopus citations

Abstract

The general context of this paper is the assessment of Sliding Mode Control (SMC) techniques for rendezvous missions in space. Based on the so called block-controllable model form, a Super-Twisting SMC is proposed in a backstepping setup. The proposed methodology is applied to a high-fidelity benchmark that accurately simulates a rendezvous mission between a chaser spacecraft and a passive target onto a circular orbit around Earth, taking into account the coupling between attitude and translational motions, propellant sloshing, modes of the flexible appendages and the most dimensioning space disturbances (e.g. second zonal harmonic J₂, atmospheric drag, magnetic disturbance). Nonlinear simulations demonstrate the potential of the proposed approach.

Original language	English
Pages (from-to)	25-30
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	52
Issue number	12
DOIs	https://doi.org/10.1016/j.ifacol.2019.11.064
State	Published - Oct 2019
Event	21st IFAC Symposium on Automatic Control in Aerospace, ACA 2019 - Cranfield, United Kingdom Duration: 27 Aug 2019 → 30 Aug 2019

Keywords

Backstepping
Rendezvous mission
Sliding mode control
Super-twisting

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10.1016/j.ifacol.2019.11.064

Cite this

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title = "A super-twisting sliding mode control in a backstepping setup for rendezvous with a passive target",

abstract = "The general context of this paper is the assessment of Sliding Mode Control (SMC) techniques for rendezvous missions in space. Based on the so called block-controllable model form, a Super-Twisting SMC is proposed in a backstepping setup. The proposed methodology is applied to a high-fidelity benchmark that accurately simulates a rendezvous mission between a chaser spacecraft and a passive target onto a circular orbit around Earth, taking into account the coupling between attitude and translational motions, propellant sloshing, modes of the flexible appendages and the most dimensioning space disturbances (e.g. second zonal harmonic J2, atmospheric drag, magnetic disturbance). Nonlinear simulations demonstrate the potential of the proposed approach.",

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author = "Torres, {Jazm{\'i}n Zenteno} and J{\'e}r{\^o}me Cieslak and David Henry and Jorge D{\'a}vila",

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AU - Dávila, Jorge

PY - 2019/10

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AB - The general context of this paper is the assessment of Sliding Mode Control (SMC) techniques for rendezvous missions in space. Based on the so called block-controllable model form, a Super-Twisting SMC is proposed in a backstepping setup. The proposed methodology is applied to a high-fidelity benchmark that accurately simulates a rendezvous mission between a chaser spacecraft and a passive target onto a circular orbit around Earth, taking into account the coupling between attitude and translational motions, propellant sloshing, modes of the flexible appendages and the most dimensioning space disturbances (e.g. second zonal harmonic J2, atmospheric drag, magnetic disturbance). Nonlinear simulations demonstrate the potential of the proposed approach.

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A super-twisting sliding mode control in a backstepping setup for rendezvous with a passive target

Abstract

Keywords

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