Fuel Optimal Control of Plane Oscillations of a Satellite on Elliptical Orbit

被引:0
|
作者
Babadzanjanz, Levon [1 ]
Pototskaya, Irina [1 ]
Alesova, Irina [1 ]
Saakyan, Artur [1 ]
机构
[1] St Petersburg State Univ, 7-9 Univ Skaya Nab, St Petersburg 199034, Russia
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Active damping of the free plane oscillations of a satellite on elliptical orbit is discussed. Satellite oscillations are described by Whittaker-Hill equation. Fuel optimal control method is offered. Numerical examples are submitted.
引用
收藏
页码:82 / 85
页数:4
相关论文
共 50 条
  • [41] PERTURBATION IN ORBITAL ELEMENTS OF A HIGH ELLIPTICAL ORBIT OF SATELLITE CONSTELLATIONS
    Mostafa, Osama
    Fujita, Koki
    Hanada, Toshiya
    SPACEFLIGHT MECHANICS 2017, PTS I - IV, 2017, 160 : 1733 - 1745
  • [42] Effect of gyroscopic moments on the attitude stability of a satellite in an elliptical orbit
    Zhao, Jie
    Zhong, Xue
    Yu, Kaiping
    Xu, Minqiang
    NONLINEAR DYNAMICS, 2023, 111 (16) : 14957 - 14976
  • [43] Effect of gyroscopic moments on the attitude stability of a satellite in an elliptical orbit
    Jie Zhao
    Xue Zhong
    Kaiping Yu
    Minqiang Xu
    Nonlinear Dynamics, 2023, 111 : 14957 - 14976
  • [44] On the Stability of Planar Oscillations and Rotations of a Satellite in a Circular Orbit
    Anatoliy P. Markeev
    Boris S. Bardin
    Celestial Mechanics and Dynamical Astronomy, 2003, 85 : 51 - 66
  • [45] Orbital stability of planar oscillations of a satellite in a circular orbit
    Bardin, B. S.
    Chekin, A. M.
    COSMIC RESEARCH, 2008, 46 (03) : 273 - 282
  • [46] Orbital stability of planar oscillations of a satellite in a circular orbit
    B. S. Bardin
    A. M. Chekin
    Cosmic Research, 2008, 46 : 273 - 282
  • [47] On the stability of planar oscillations and rotations of a satellite in a circular orbit
    Markeev, AP
    Bardin, BS
    CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2003, 85 (01): : 51 - 66
  • [48] OSCILLATIONS OF A SATELLITE WITH COMPENSATING DEVICES IN AN ELLIPTIC ORBIT.
    Polyanskaya, I.P.
    Cosmic Research (English translation of Kosmicheskie Issledovaniya), 1982, 20 (05): : 474 - 480
  • [49] Fuel-optimal precise rendezvous guidance law in elliptical reference orbit with J2 perturbation
    Jing W.
    Chen W.
    Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology, 2011, 31 (02): : 16 - 24+78
  • [50] Symmetric oscillations of charged gyrostat in weakly elliptical orbit with small inclination
    Tikhonov, A. A.
    Tkhai, V. N.
    NONLINEAR DYNAMICS, 2016, 85 (03) : 1919 - 1927