On Analytical Investigation and Computer Modeling of Spacecraft Nonlinear Resonance Oscillations

Links

http://www.scopus.com/inward/record.url?eid=2-s2.0-84908680665&partnerID=40&md5=50e9b13f8dcee6549f42901139627e8d

DOI

https://doi.org/10.1109/ICCTPEA.2014.6893287
Other version

E.A. Kosjakov
I.E. Murzinov
A.A. Tikhonov

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.

Original language	English
Title of host publication	2014 INTERNATIONAL CONFERENCE ON COMPUTER TECHNOLOGIES IN PHYSICAL AND ENGINEERING APPLICATIONS (ICCTPEA)
Editors	EI Veremey
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	74-74
Number of pages	1
ISBN (Print)	9781479953172
DOIs	https://doi.org/10.1109/ICCTPEA.2014.6893287
State	Published - 2014
Event	International Conference on Computer Technologies in Physical and Engineering Applications (ICCTPEA) - Saint Petersburg, Russian Federation Duration: 30 Jun 2014 → 4 Jul 2014 http://www.ivesc2014.com/

Conference

Conference	International Conference on Computer Technologies in Physical and Engineering Applications (ICCTPEA)
Country/Territory	Russian Federation
City	Saint Petersburg
Period	30/06/14 → 4/07/14
Internet address	http://www.ivesc2014.com/

ID: 7018853