From a system engineering point of view, there are several fundamental concepts for three-axis attitude and momentum control, which are briefly discussed in the first section. It concludes with an overview of the most common control tasks in satellite attitude control. In the remaining part of the chapter, common control approaches for attitude and angular momentum control are explained in detail, together with a formulation and discussion of the closed loop systems.
Attitude and Momentum Control
Principles of Spacecraft Control ; Kapitel : 5 ; 115-154
16.04.2022
40 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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