DocumentCode
229327
Title
On analytical investigation and computer modeling of spacecraft nonlinear resonance oscillations
Author
Kosjakov, E.A. ; Murzinov, I.E. ; Tikhonov, A.A.
Author_Institution
St.-Petersburg State Univ., St. Petersburg, Russia
fYear
2014
fDate
June 30 2014-July 4 2014
Firstpage
74
Lastpage
74
Abstract
Oscillatory attitude motion of a gravity-oriented spacecraft is considered. A special notation for differential equations of perturbed librational motion of the spacecraft is derived. The derived equations are convenient for the analysis of nonlinear resonance oscillations with the use of asymptotic methods and allow to obtain some new results.
Keywords
approximation theory; differential equations; oscillations; space vehicles; spacecraft computers; analytical investigation; asymptotic method; computer modeling; differential equations; gravity-oriented spacecraft; oscillatory attitude motion; perturbed librational motion; spacecraft nonlinear resonance oscillations; Differential equations; Educational institutions; Equations; Mathematical model; Oscillators; Space vehicles; Torque;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Technologies in Physical and Engineering Applications (ICCTPEA), 2014 International Conference on
Conference_Location
St. Petersburg
Print_ISBN
978-1-4799-5315-8
Type
conf
DOI
10.1109/ICCTPEA.2014.6893287
Filename
6893287
Link To Document