Анализ взаимной эволюции параметров двух синхронно прецессирующих орбит
Инженерный журнал: наука и инновации
# 3·2016 15
Analysis of the mutual evolution of the parameters
of two synchronous precessing orbits
©
S.Yu. Ulybyshev
FSUE Central Research and Development Institute of Chemistry and Mechanics
named after D.I. Mendeleev, Moscow, 115487, Russia
The article considers the analysis of the mutual evolution of the two nominally
synchronous precessing low-ellipticity orbits. The recommendations about the
parameters of the being formed synchronous precessing orbit (SPO) in order to minimize
the characteristic speed loss for its maintenance and ensuring the eventual transition into
a working orbit are developed. The analysis of the necessary precision of knowledge of
the orbit parameters for long-term forecasting and planning SPO correction dates as
well as the need for their implementation was performed.
Keywords:
orbits synchronization,
spatial angle, planes of the orbits
, orbit with
synchronous recession, TLE.
REFERENCES
[1]
Barinov K.N., Burdaev M.N., Mamon P.A.
Dinamika i printsipy postroeniya
orbitalnykh system kosmicheskikh apparatov
[Dynamics and the Principles of
Orbital Spacecraft System Constructing]. Moscow, Mashinostroenie Publ.,
1975.
[2]
Mozhaev G.V.
Kosmicheskie issledovaniya — Cosmic Research
, 1972, vol. 10,
no. 6, pp. 833–843; 1973, vol. 11, no. 1, pp. 59–68.
[3]
Dudnikov V.N.
Issledovanie nekotorykh voprosov postroeniya system
kruglosutochnoy radiosvyazi s ispolzovaniem iskusstvennykh sputnikov Zemli
Molniya 1. Avtoreferat Diss. cand. tekhn. nauk
[Investigation of Some Questions
of Developing Round-the-Clock Radio Communication Systems Using Earth
Artificial Satellites Molniya-1. Abstract Cand. Eng. Sci. Diss.]. Moscow, 1968.
[4]
Lang T.J., Adams W.S. A Comparison of Satellite Constellations for Continuous
Global Coverage.
IAF Workshop on Mission Design and Implementation of
Satellite Constellations. Toulouse (France)
, 1997, р. 97–D4. Available at:
http://www.springer.com/us/book/9780792352105[5]
Ulybyshev
S.Yu., Doniants V.N., et al.
Sputnikovaya cictema regionalnoy svyazi
s ispolzovaniem ellipticheskikh orbit
[Regional satellite communication system
using elliptical orbits]. Patent RF, no. 2149507, IPC H04B7/185. Available at:
http://www.fips.ru[6]
Baranov A.A., Burdyanskiy A.A., Chernov N.V.
Kosmicheskie issledovaniya —
Cosmic Research
, 2015, vol. 53, pp. 409–413.
Ulybyshev
S.Yu.
(b. 1986) graduated from Bauman Moscow State Technical University
in 2009. Cand. Sci. (Eng.), lead engineer at FSUE Central Research and Development
Institute of Chemistry and Mechanics named after D.I. Mendeleev. Author of more than
10 papers on calculation of the trajectories of spacecraft launch, driving dynamics of
manned reentry vehicles in case of emergencies and on designing satellite systems.
e-mail:
wardoc5@rambler.ru