A new variant of the B-dot control for spacecraft magnetic detumbling
Document Type
Article
Publication Date
6-2020
Department
Department of Mechanical Engineering-Engineering Mechanics
Abstract
With using the B-dot control law for magnetic detumbling, there will be no need for angular velocity measurements. The B-dot control law is a torque projection-based controller, however, it is not guaranteed to have the dipole moment orthogonal to the magnetic field, especially as the angular velocity gets smaller during detumbling, resulting in a suboptimal torque vector. This paper presents a new variant of the B-dot control. By computing an equivalent angular velocity, based on the magnetic field data, it is possible to develop a control law that guarantees the magnetic dipole moment to remain in the plane orthogonal to the ambient magnetic field. Using Monte Carlo simulations, the proposed B-dot control is compared to two other variants of B-dot control laws: a simple B-dot control and a recent variable gain B-dot control. The results show that the proposed B-dot control outperforms the other B-dot control laws in terms of the speed of detumbling and the power consumption.
Publication Title
Acta Astronautica
Recommended Citation
Desouky, M.,
&
Abdelkhalik, O.
(2020).
A new variant of the B-dot control for spacecraft magnetic detumbling.
Acta Astronautica,
171, 14-22.
http://doi.org/10.1016/j.actaastro.2020.02.030
Retrieved from: https://digitalcommons.mtu.edu/michigantech-p/1764