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]
Cite
CITATION STYLE
APA
Ramnath, R. V. (2012). Satellite attitude control. SpringerBriefs in Applied Sciences and Technology, (9783642257483), 93–110. https://doi.org/10.1007/978-3-642-25749-0_8
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