Robust parametric control of spacecraft rendezvous
type: Item
instance of: scholarly article
title: Robust parametric control of spacecraft rendezvous
zbMATH Open document ID: 1407.93284
DOI: 10.1155/2014/961367
published in: Mathematical Problems in Engineering
publication date: 2019-02-08T00:00:00Z
review text: Summary: This paper proposes a method to design the robust parametric control for autonomous rendezvous of spacecrafts with the inertial information with uncertainty. We consider model uncertainty of traditional C-W equation to formulate the dynamic model of the relative motion. Based on eigenstructure assignment and model reference theory, a concise control law for spacecraft rendezvous is proposed which could be fixed through solving an optimization problem. The cost function considers the stabilization of the system and other performances. Simulation results illustrate the robustness and effectiveness of the proposed control.
Mathematics Subject Classification ID: 93C95
Mathematics Subject Classification ID: 93D21
Mathematics Subject Classification ID: 93C15
zbMATH DE Number: 7017719
author: Da-Ke Gu
author: Yin-Dong Liu
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.1155/2014/961367
OpenAlex ID: W1978436686
Wikidata QID: Q59071177
cites work: Q3273009
cites work: Solutions of the equation AV+BW=VF and their application to eigenstructure assignment in linear systems
description: scientific article; zbMATH DE number 7017719