A heuristic design method for attitude stabilization of magnetic actuated satellites-Reference-Cited by-同舟云学术

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A heuristic design method for attitude stabilization of magnetic actuated satellites

Published:2009-12 Issue:11-12 Volume:65 Page:1813-1825
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Bayat Farhad,Bolandi Hossein,Jalali Ali A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. Rate damping control for small satellite using thruster;Weidong;Acta Astronautica,2004

2. Fully magnetic attitude control for spacecraft subject to gravity gradient;Wisniewski;Automatica,1999

3. Attitude stabilization of a satellite by magnetic coils;Bushenkov;Acta Astronautica,2002

4. The attitude control problem;Wen;IEEE Transactions on Automatic Control,1991

5. Comments on the attitude control problem;Fjellstad;IEEE Transactions on Automatic Control,1994

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1. Model Predictive Sliding Control for Finite-Time Three-Axis Spacecraft Attitude Tracking;IEEE Transactions on Industrial Electronics;2019-10

2. A survey on active magnetic attitude control algorithms for small satellites;Progress in Aerospace Sciences;2019-08

3. Attitude control of Low Earth Orbit satellites by reaction wheels and magnetic torquers;Acta Astronautica;2019-07

4. Two‐Layer Terminal Sliding Mode Attitude Control of Satellites Equipped with Reaction Wheels;Asian Journal of Control;2018-07-30

5. On the monoaxial stabilization of a rigid body under vanishing restoring torque;AIP Conference Proceedings;2018

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