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