Orbit design for the Spektr-R spacecraft of the ground-space interferometer

被引：6
作者：
Kardashev, N. S. [1 ]
Kreisman, B. B. [1 ]
Pogodin, A. V. [2 ]
Ponomarev, Yu N. [1 ]
Filippova, E. N. [2 ]
Sheikhet, A. I. [2 ]
机构：
[1] Russian Acad Sci, PN Lebedev Phys Inst, Astrospace Ctr, Moscow, Russia
[2] Lavochkin NPO Sci & Prod Corp, Chimki, Moscow Oblast, Russia
来源：
COSMIC RESEARCH | 2014年 / 52卷 / 05期
关键词：
Cosmic Research; Orbit Evolution; Orbit Design; Space Radio Telescope; Perigee Height;
D O I：
10.1134/S0010952514050050
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In order to carry out tasks of the RadioAstron mission, a high-apogee orbit was designed. On average, the period of its satellite's orbit around the Earth is 8.5 days with evolution due to gravitational perturbations produced by the Moon and the Sun. The perigee and apogee of this orbit vary within the limits 7500-70000 km and 270000-333000 km, respectively. The basic evolution of the orbit represents a rotation of its plane around the line of apsides. Over 3 years, the plane normal to the orbit draws on the celestial sphere an oval with a semi-major axis of about 150A degrees and semi-minor axis of about 45A degrees.
引用
收藏
页码：332 / 341
页数：10
相关论文
共 11 条
  • [1] Orbit design for the Spektr-R spacecraft of the ground-space interferometer
    N. S. Kardashev
    B. B. Kreisman
    A. V. Pogodin
    Yu. N. Ponomarev
    E. N. Filippova
    A. I. Sheikhet
    Cosmic Research, 2014, 52 : 332 - 341
  • [2] Trajectory correction of the Spektr-R spacecraft motion
    G. S. Zaslavskiy
    V. A. Stepan’yants
    A. G. Tuchin
    A. V. Pogodin
    E. N. Filippova
    A. I. Sheikhet
    Cosmic Research, 2014, 52 : 353 - 364
  • [3] Trajectory correction of the Spektr-R spacecraft motion
    Zaslavskiy, G. S.
    Stepan'yants, V. A.
    Tuchin, A. G.
    Pogodin, A. V.
    Filippova, E. N.
    Sheikhet, A. I.
    COSMIC RESEARCH, 2014, 52 (05) : 353 - 364
  • [4] Orbit design for hybrid ground-space targets
    Zhang, Haiyang
    Zhang, Gang
    Tian, Longfei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 129
  • [5] Analysis of SPEKTR-R spacecraft operating modes for various algorithms of high gain antenna drive control
    Telepnev, P. P.
    Efanov, V. V.
    Kuznetsov, D. A.
    Ermakov, V. Yu.
    SOLAR SYSTEM RESEARCH, 2015, 49 (07) : 610 - 613
  • [6] Analysis of SPEKTR-R spacecraft operating modes for various algorithms of high gain antenna drive control
    P. P. Telepnev
    V. V. Efanov
    D. A. Kuznetsov
    V. Yu. Ermakov
    Solar System Research, 2015, 49 : 610 - 613
  • [7] Orbit Design for Twin-spacecraft Space VLBI
    ZHANG Cheng
    WU Xia
    ZHENG Jianhua
    WU Ji
    空间科学学报, 2015, 35 (04) : 502 - 510
  • [8] Orbit design for the Laser Interferometer Space Antenna (LISA)
    Yan Xia
    GuangYu Li
    Gerhard Heinzel
    Albrecht Rüdiger
    YongJie Luo
    Science China Physics, Mechanics and Astronomy, 2010, 53 : 179 - 186
  • [9] Orbit design for the Laser Interferometer Space Antenna (LISA)
    Gerhard HEINZEL
    Albrecht RDIGER
    Science China(Physics,Mechanics & Astronomy), 2010, (01) : 179 - 186
  • [10] Orbit design for space atom-interferometer AIGSO
    Wang, Gang
    Gao, Dongfeng
    Ni, Wei-Tou
    Wang, Jin
    Zhan, Mingsheng
    INTERNATIONAL JOURNAL OF MODERN PHYSICS D, 2020, 29 (04):
12