| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1714216 | Acta Astronautica | 2016 | 4 Pages |
Abstract
Satellite equipped with purely magnetic attitude control system is considered. Sliding mode control is used to achieve three-axis satellite attitude. Underactuation problem is solved for transient motion. Necessary attitude is acquired by proper sliding manifold construction. Satellite motion on the manifold is executed with magnetic control system. One manifold construction approach is proposed and discussed. Numerical examples are provided.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
M.Yu. Ovchinnikov, D.S. Roldugin, V.I. Penkov, S.S. Tkachev, Y.V. Mashtakov,