Averaging Methods for Design of Spacecraft Hysteresis Damper-Reference-Cited by-同舟云学术

Averaging Methods for Design of Spacecraft Hysteresis Damper

Published:2013 Issue: Volume:2013 Page:1-7
ISSN:1024-123X
Container-title:Mathematical Problems in Engineering
language:en
Short-container-title:Mathematical Problems in Engineering

Author:

Gama Ricardo¹^ORCID,Guerman Anna D.²,Seabra Ana³^ORCID,Smirnov Georgi V.⁴

Affiliation:

1. School of Technology and Management of Lamego, Avenida Visconde Guedes Teixeira, 5100-074 Lamego, Portugal

2. Centre for Aerospace Science and Technologies, University of Beira Interior, Calçada Fonte do Lameiro, 6201-001 Covilhã, Portugal

3. Scientific Area of Mathematics, ESTGV, Polytechnic Institute of Viseu, Campus Politécnico, 3504-510 Viseu, Portugal

4. Centre of Physics, Department of Mathematics and Applications, University of Minho, Campus de Gualtar, 4710-057 Braga, Portugal

Abstract

This work deals with averaging methods for dynamics of attitude stabilization systems. The operation of passive gravity-gradient attitude stabilization systems involving hysteresis rods is described by discontinuous differential equations. We apply recently developed averaging techniques for discontinuous system in order to simplify its analysis and to perform parameter optimization. The results obtained using this analytic method are compared with those of numerical optimization.

Funder

Fundação para a Ciência e a Tecnologia

Publisher

Hindawi Limited

Subject

General Engineering,General Mathematics

Link

http://downloads.hindawi.com/journals/mpe/2013/483457.pdf

Reference16 articles.

1. Attitude control system for the first swedish nanosatellite “MUNIN”

2. Passive magnetic attitude stabilization of the UNISAT-4 microsatellite

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