Academy Transaction note “matrix gains selection for three-axis magnetic attitude control of dynamically elongated satellite”-Reference-Cited by-同舟云学术

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Academy Transaction note “matrix gains selection for three-axis magnetic attitude control of dynamically elongated satellite”

Published:2024-11 Issue: Volume:224 Page:445-448
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Monakhova Uliana^ORCID,Mashtakov Yaroslav^ORCID,Ivanov Danil^ORCID,Ovchinnikov Mikhail^ORCID

Funder

Russian Science Foundation

Publisher

Elsevier BV

Reference12 articles.

1. Choosing control parameters for three axis magnetic stabilization in orbital frame;Ovchinnikov;Acta Astronaut.,2015

2. A robust optimization approach for magnetic spacecraft attitude stabilization;Bruni;J. Optim. Theor. Appl.,2017

3. Hybrid magnetic attitude control gain selection;Damaren;Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.,2009

4. Attitude determination & control system design for gravity recovery missions like GRACE;Mashtakov;Acta Astronaut.,2020

5. Magnetic torquer attitude control via asymptotic periodic linear quadratic regulation;Psiaki;J. Guid. Control Dynam.,2001

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