Robust tracking control for rendezvous in near-circular orbits
type: Item
instance of: scholarly article
title: Robust tracking control for rendezvous in near-circular orbits
zbMATH Open document ID: 1299.93204
DOI: 10.1155/2013/726945
author: Neng Wan
author: Ming Liu
author: Hamid Reza Karimi
published in: Mathematical Problems in Engineering
publication date: 2014-11-24T00:00:00Z
review text: Summary: This paper investigates a robust guaranteed cost tracking control problem for thrust-limited spacecraft rendezvous in near-circular orbits. Relative motion model is established based on the two-body problem with noncircularity of the target orbit described as a parameter uncertainty. A guaranteed cost tracking controller with input saturation is designed via a linear matrix inequality (LMI) method, and sufficient conditions for the existence of the robust tracking controller are derived, which is more concise and less conservative compared with the previous works. Numerical examples are provided for both time-invariant and time-variant reference signals to illustrate the effectiveness of the proposed control scheme when applied to the terminal rendezvous and other astronautic missions with scheduled states signal.
Mathematics Subject Classification ID: 93C95
Mathematics Subject Classification ID: 93D09
zbMATH DE Number: 6373005
Wikidata QID: Q59028662
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.1155/2013/726945
OpenAlex ID: W2094604502
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description: scientific article; zbMATH DE number 6373005