Abstract
The physical environment of a space vehicle shows that bang-bang method for attitude control system of a space vehicle is a viable and natural choice. This tutorial describes the algorithm and the specific aspects of its implementation. It derives the equations and the switching surface used by the method. The immediate benefits of this design is short response time which results in larger fuel margin, less fuel consumption and less weight.
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Authors
Esmat C. Bekir
Topics
Inertial Sensor and NavigationSpace Satellite Systems and Control
About
PublishedDec 30, 2018
TypeArticle
Citations1