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Satellite Attitude Control

  • Rudrapatna V. Ramnath
Chapter
Part of the SpringerBriefs in Applied Sciences and Technology book series (BRIEFSAPPLSCIENCES)

Abstract

This chapter presents another example in space flight showing the computational advantages of asymptotic solutions. This application involves the attitude control of a dual spin satellite in an earth orbit by utilizing the interaction of an on-board electromagnet with the geomagnetic field. The presentation is based on [1, 2]

Keywords

Roll Angle Control Torque High Frequency Part Pitch Axis Direct Numerical Solution 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

References

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Copyright information

© The Author(s) 2012

Authors and Affiliations

  1. 1.Massachusetts Institute of TechnologyLexingtonUSA

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