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.
Primary Language | English |
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Journal Section | Articles |
Authors | |
Publication Date | December 30, 2018 |
Submission Date | September 6, 2018 |
Acceptance Date | November 14, 2018 |
Published in Issue | Year 2018 Volume: 1 Issue: 2 |
An international scientific e-journal published by the University of Usak