Choosing control parameters for three axis magnetic stabilization in orbital frame-Reference-Cited by-同舟云学术

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Choosing control parameters for three axis magnetic stabilization in orbital frame

Published:2015-11 Issue: Volume:116 Page:74-77
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ovchinnikov M.Yu.,Roldugin D.S.,Ivanov D.S.,Penkov V.I.

Funder

RFBR

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference4 articles.

1. Three-axis active magnetic attitude control asymptotical study,;Ovchinnikov;Acta Astronaut.,2015

2. Active magnetic attitude control system providing three-axis inertial attitude;Ovchinnikov;Keldysh Inst. Prepr.,2013

3. I.G. Malkin, Theory of Stability of Motion. Oak Ridge: U.S. Atomic Energy Commission, Technical Information Service, 1952.

4. Three-axis satellite stabilization using only magnetorquers and magnetometer;Ivanov;Keldysh Inst. Prepr.,2015

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2. Comparative Cost Functions Analysis in the Construction of a Reference Angular Motion Implemented by Magnetorquers;Aerospace;2023-05-17

3. Academy transaction note “closed form solution for a minimum deviation magnetically controllable satellite angular trajectory”;Acta Astronautica;2023-02

4. A Recursive Approach for Magnetic Field Estimation in Spacecraft Magnetic Attitude Control;Aerospace;2022-12-15

5. Application of a PID-like control to the problem of triaxial electrodynamic attitude stabilization of a satellite in the orbital frame;Aerospace Science and Technology;2022-08

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