Methods of Accounting for the Shadow Zones Influence on Low Thrust Spacecraft Moving in the Earth - Moon System

被引：0
作者：
Faim, M. [1 ]
机构：
[1] Samara Univ, Samara Natl Res Univ, Samara 443086, Russia
来源：
XLIII ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S P KOROLEV AND OTHER OUTSTANDING RUSSIAN SCIENTISTS - PIONEERS OF SPACE EXPLORATION | 2019年 / 2171卷
关键词：
NON-KEPLERIAN ORBITS; OPTIMIZATION; TRAJECTORIES;
D O I：
10.1063/1.5133310
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
The article considers mathematical model of the light-to-dark situation in the Earth-Moon system and its influence on controlling the motion of a spacecraft equipped with low-thrust engines. All transfers were analyzed within the framework of the limited three-body problem. Mathematical model of spacecraft transfers between L1 and L2 libration points is described in the barycentric coordinate system. Disturbances originating from the Earth, the Moon and the Sun were taken into account and included polar compression of the Earth and the Moon, oscillations of the Earth around the barycenter, influence of other planets of the Solar system, inclination of the Moon's plane to the mean plane of the Moon, as well as shadow zones created by the Earth and the Moon. The optimal control program was obtained using the Fedorenko sequential linearization method for finding the derivatives and the gradient method for optimizing control laws. As a result of optimization, control laws corresponding to trajectory and values of the total transfer time duration were obtained.
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页数：7
相关论文
共 16 条
  • [1] Andrews D. G., 2005, AIAA SPAC 2005 C EXH
  • [2] [Anonymous], 2015, MARS ORB MISS
  • [3] Optimal low thrust trajectories to the moon
    Betts, JT
    Erb, SO
    [J]. SIAM JOURNAL ON APPLIED DYNAMICAL SYSTEMS, 2003, 2 (02): : 144 - 170
  • [4] Selection of Luna-25 landing sites in the South Polar Region of the Moon
    Djachkova, M. V.
    Litvak, M. L.
    Mitrofanov, I. G.
    Sanin, A. B.
    [J]. SOLAR SYSTEM RESEARCH, 2017, 51 (03) : 185 - 195
  • [5] Fain MK, 2015, 2015 7TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST), P95, DOI 10.1109/RAST.2015.7208322
  • [6] Grossman Y., 2017, LUNAR PLANETARY SCI, VXLVIII
  • [7] Hashimoto T., 2017, LUNAR POLAR EXPLORAT
  • [8] COMPARISON OF POTENTIAL ELECTRIC PROPULSION SYSTEMS FOR ORBIT TRANSFER
    JONES, RM
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1984, 21 (01) : 88 - 95
  • [9] Method for optimization of trajectories including gravitational maneuvers of a spacecraft with a solar sail
    Kazmerchuk, P. V.
    Malyshev, V. V.
    Usachev, V. E.
    [J]. JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2007, 46 (01) : 150 - 161
  • [10] Loeb H.W., 2011, 32 INT EL PROP C WIE
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