Perturbation Effects in Orbital elements of CubeSats

被引:0
|
作者
Hanafi, Ahmed [1 ]
Karim, Mohammed [1 ]
Hachem, El-Kaber [2 ]
Rachidi, Tajjeeddine [3 ]
Sahmoudi, Mohamed [4 ]
机构
[1] FSDM, LISTA Lab, Fes, Morocco
[2] UMI, Dept Phys, Fac Sci, Meknes, Morocco
[3] Al Akhawayn Univ, Dept Comp Sci, Ifrane, Morocco
[4] Higher Inst Aeronaut & Space, Toulouse, France
关键词
Orbit perturbations; CubeSat; Keplerian Orbital elements;
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
The main objective of this paper is to evaluate the perturbations in CubeSat's orbital elements in low Earth orbits (LEO) using the Cowell's method. The disturbing forces are driving the satellite (the satellite's trajectory) away from Keplerian orbit, therefore produce a change in Keplerian orbital elements over time. In this paper, after introducing the perturbing forces acting on a satellite in LEO, the methods of converting the orbital elements into state vector and the opposite are being presented, and in the end, the perturbations in orbital elements of CubeSats in LEO are evaluated.
引用
收藏
页码:397 / 402
页数:6
相关论文
共 50 条
  • [1] Perturbation Effects of Quadratic Drag on the Orbital Elements of a Satellite in a Central Force Field
    Li, Lin-Sen
    JOURNAL OF THE ASTRONAUTICAL SCIENCES, 2011, 58 (01): : 23 - 33
  • [2] Perturbation Effects of Quadratic Drag on the Orbital Elements of a Satellite in a Central Force Field
    Lin-Sen Li
    The Journal of the Astronautical Sciences, 2011, 58 : 23 - 33
  • [3] A test on GPS orbital parameters and perturbation elements
    Xie, P
    Du, XJ
    Li, HJ
    Xie, H
    ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 8860 - 8863
  • [4] ELECTRIC MICROPROPULSION FOR ORBITAL CONTROL OF CUBESATS
    Gamero-Castano, Manuel
    Villac, Benjamin F.
    GUIDANCE AND CONTROL 2009, 2009, 133 : 561 - 568
  • [5] 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
  • [6] ORBITAL PERTURBATION EFFECTS IN BETA-DECAY
    SCHWARTZ, HM
    EDWARDS, RR
    JOURNAL OF CHEMICAL PHYSICS, 1951, 19 (03): : 385 - 386
  • [7] The Perturbation Effect of Rotating Solar Polytropic Model on the Variation of Planetary Orbital Elements
    Li, L.-S.
    Communications in Theoretical Physics, 27 (03):
  • [8] The perturbation effect of rotating solar polytropic model on the variation of planetary orbital elements
    Li, LS
    COMMUNICATIONS IN THEORETICAL PHYSICS, 1997, 27 (03) : 361 - 366
  • [9] Perturbation effect of the Coulomb drag on the orbital elements of the earth satellite moving in the ionosphere
    Li, Lin-Sen
    ACTA ASTRONAUTICA, 2011, 68 (7-8) : 717 - 721
  • [10] Orbital Maintenance of a Constellation of CubeSats for Internal Gravity Wave Tomography
    Leroy, Stephen
    Fitzgerald, Riley
    Cahoy, Kerri
    Abel, James
    Clark, James
    IEEE JOURNAL OF SELECTED TOPICS IN APPLIED EARTH OBSERVATIONS AND REMOTE SENSING, 2020, 13 : 307 - 317