DocumentCode :
646557
Title :
Detumbling of highly non-symmetrical satellites with use of B-dot control law
Author :
Juchnikowski, Grzegorz ; Barcinski, Tomasz ; Lisowski, Jakub
Author_Institution :
Space Res. Centre, Warsaw, Poland
fYear :
2013
fDate :
26-29 Aug. 2013
Firstpage :
582
Lastpage :
587
Abstract :
Presented are results of simulations of B-dot detumbling for satellites with different types of non-symmetrical mass distributions. Results are next compared with the theoretical derivation of the problem made for the case of spherically symmetrical bodies.
Keywords :
artificial satellites; attitude control; B-dot control law; B-dot detumbling; highly nonsymmetrical satellites; nonsymmetrical mass distributions; spherically symmetrical bodies; Magnetic separation; Magnetomechanical effects; Magnetosphere; Orbits; Satellites; Torque; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Methods and Models in Automation and Robotics (MMAR), 2013 18th International Conference on
Conference_Location :
Miedzyzdroje
Print_ISBN :
978-1-4673-5506-3
Type :
conf
DOI :
10.1109/MMAR.2013.6669975
Filename :
6669975
Link To Document :
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