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Nonlinear Controller Design for a Flexible Spacecraft

Redondo Gutierrez, Jose Luis and Heidecker, Ansgar (2020) Nonlinear Controller Design for a Flexible Spacecraft. Journal of the Astronautical Sciences. American Astronautical Society. doi: 10.1007/s40295-020-00234-z. ISSN 0021-9142.

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Official URL: https://link.springer.com/journal/40295

Abstract

This paper combines the nonlinear Udwadia-Kalaba control approach with the Assumed Mode Method to model flexible structures and derives an attitude controller for a spacecraft. The study case of this paper is a satellite with four flexible cantilever beams attached to a rigid central hub. Two main topics are covered in this paper. The first one is the formulation of the equation of motion and the second one is the nonlinear controller design. The combination of these two techniques is able to provide a controller that damps the vibration of a flexible structure while achieving the desired rigid-motion state.

Item URL in elib:https://elib.dlr.de/135766/
Document Type:Article
Title:Nonlinear Controller Design for a Flexible Spacecraft
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Redondo Gutierrez, Jose LuisJose.RedondoGutierrez (at) dlr.dehttps://orcid.org/0000-0002-0037-2299
Heidecker, AnsgarAnsgar.Heidecker (at) dlr.dehttps://orcid.org/0000-0002-7483-9074
Date:23 October 2020
Journal or Publication Title:Journal of the Astronautical Sciences
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.1007/s40295-020-00234-z
Publisher:American Astronautical Society
ISSN:0021-9142
Status:Published
Keywords:attitude control, non-linear control, flexible satellites, active damping, Udwadia-Kalaba
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Systemtechnologien (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Heidecker, Dipl.-Ing. Ansgar
Deposited On:27 Oct 2020 08:58
Last Modified:01 Jan 2023 03:00

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