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The B-dot Earth Average Magnetic FieldThe average Earth's magnetic field is solved with complex mathematical models based on mean square integral. Depending on the selection of the Earth magnetic model, the average Earth's magnetic field can have different solutions. This paper presents a simple technique that takes advantage of the damping effects of the b-dot controller and is not dependent of the Earth magnetic model; but it is dependent on the magnetic torquers of the satellite which is not taken into consideration in the known mathematical models. Also the solution of this new technique can be implemented so easily that the flight software can be updated during flight, and the control system can have current gains for the magnetic torquers. Finally, this technique is verified and validated using flight data from a satellite that it has been in orbit for three years.
Document ID
20140016484
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Capo-Lugo, Pedro A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rakoczy, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sanders, Devon
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 20, 2014
Publication Date
January 1, 2013
Subject Category
Geophysics
Spacecraft Design, Testing And Performance
Report/Patent Number
M13-2829
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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