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 :
بازگشت