ANALYSIS OF THE EFFECTS OF ELECTROMAGNETIC FORCES ON THE RELATIVE MOTION OF A CHARGED SPACECRAFT FORMATION FLYING

被引:0
|
作者
Tealib, Shafeeq Kaheal [1 ]
Abdel-Aziz, Yehia [1 ]
Awad, Mervat El-Said [2 ]
Khalil, Khalil Ibrahim [1 ]
Radwan, Mohmed [2 ]
机构
[1] Natl Res Inst Astron & Geophys, Cairo, Egypt
[2] Cairo Univ, Fac Sci, Cairo, Egypt
来源
关键词
electromagnetic forces; formation flying; relative motion; a charged spacecraft; LORENTZ; SATELLITE; DYNAMICS; ORBIT;
D O I
10.2478/arsa-2020-0007
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
In recent years, studying Lorentz's force has become a possible good means to control the spacecraft to reduce the fuel cost by modulating spacecraft electrostatic charge (magnetic and electric fields). The generation of Lorentz force is finite by the natural magnetic field and the relative velocity of the spacecraft. Therefore, the Lorentz force cannot fully occur from conventional propulsion technologies. Previous studies are concerned with studying Lorentz's strength in the magnetic field only. In this work, we developed a mathematical model for a new technique establishing a raise in the level of charging in the spacecraft surface that is moving in the Earth's magnetic field and provided by modulating spacecraft's electrostatic charge that induces acceleration via the Lorentz force. The acceleration will be used to find the relationship between capacitance and power required to minimize the consumption of control energy used in such cases or to replace the usual control thruster by Lorentz force.
引用
收藏
页码:87 / 99
页数:13
相关论文
共 50 条
  • [1] Comparison of Relative Motion Models for Spacecraft Flying in Formation
    Suslova I.A.
    Mashtakov Y.V.
    Shestakov S.A.
    [J]. Mathematical Models and Computer Simulations, 2023, 15 (1) : 47 - 58
  • [2] Electromagnetic effects on the orbital motion of a charged spacecraft
    Abdel-Aziz, Yehia Ahmed
    Khalil, Khalil Ibrahim
    [J]. RESEARCH IN ASTRONOMY AND ASTROPHYSICS, 2014, 14 (05) : 589 - 600
  • [3] Electromagnetic effects on the orbital motion of a charged spacecraft
    Yehia Ahmed Abdel-Aziz
    Khalil Ibrahim Khalil
    [J]. Research in Astronomy and Astrophysics, 2014, 14 (05) : 589 - 600
  • [4] Relative trajectory analysis of dissimilar formation flying spacecraft
    Balaji, SK
    Tatnall, AR
    [J]. SPACEFLIGHT MECHANICS 2003, PTS 1-3, 2003, 114 : 531 - 543
  • [5] Relative navigation for spacecraft formation flying
    Hartman, KR
    Gramling, CJ
    Lee, T
    Kelbel, DA
    Long, AC
    [J]. SPACEFLIGHT DYNAMICS 1998, VOL 100, PART 1 AND 2, 1998, 100 : 685 - 699
  • [6] Application of Analytic Solution in Relative Motion to Spacecraft Formation Flying in Elliptic Orbit
    Cho, Hancheol
    Park, Sang-Young
    Choi, Kyu-Hong
    [J]. JOURNAL OF ASTRONOMY AND SPACE SCIENCE, 2008, 25 (03) : 255 - 266
  • [7] Relative motion coupled control for formation flying spacecraft via convex optimization
    Wu, Yun-Hua
    Cao, Xi-Bin
    Xing, Yan-Jun
    Zheng, Peng-Fei
    Zhang, Shi-Jie
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2010, 14 (06) : 415 - 428
  • [8] Spacecraft formation flying using Lorentz forces
    Peck, M. A.
    Streetman, B.
    Saaj, C. M.
    Lappas, V.
    [J]. JBIS-JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY, 2007, 60 (07): : 263 - 267
  • [9] Spacecraft formation flying and reconfiguration with electrostatic forces
    Lappas, Vaios
    Saaj, Chakravarthini
    Richie, Dave
    Peck, Mason
    Streetman, Brett
    Schaub, Hanspeter
    [J]. SPACE FLIGHT MECHANICS 2007, VOL 127, PTS 1 AND 2, 2007, 127 : 217 - +
  • [10] Relative navigation for autonomous formation flying of spacecraft
    Gramling, CJ
    Lee, T
    Niklewski, DJ
    Long, AC
    [J]. ASTRODYNAMICS 1997, 1998, 97 : 435 - 450