International Journal of Astronomy and Astrophysics

International Journal of Astronomy and Astrophysics

ISSN Print: 2161-4717
ISSN Online: 2161-4725
www.scirp.org/journal/ijaa
E-mail: ijaa@scirp.org
"Halo Orbits around Sun-Earth L1 in Photogravitational Restricted Three-Body Problem with Oblateness of Smaller Primary"
written by Prithiviraj Chidambararaj, Ram Krishan Sharma,
published by International Journal of Astronomy and Astrophysics, Vol.6 No.3, 2016
has been cited by the following article(s):
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[1] Generation of Artificial Halo Orbits in Near-Moon Space Using Low-Thrust Engines
Cosmic Research, 2022
[2] Halo orbits around , , and in the photogravitational Sun–Mars elliptical restricted three-body problem
Astrophysics and Space Science, 2022
[3] Effects of mass ratio on halo orbits about L1 and L2
AIP Conference Proceedings, 2022
[4] Infinitesimal Orbit Dynamics around Equilibrium Points in the Oblate RTBP
Bar - The Journal of the Astronautical Sciences, 2021
[5] Fifth order solution of halo orbits via Lindstedt–Poincaré technique and differential correction method
2021
[6] Halo Orbits around and in the Photogravitational Sun-Earth System with Oblateness
2020
[7] Formation flight design using natural dynamics for halo orbiting and earth orbiting spacecraft
2020
[8] Stationary solutions, critical mass, Tadpole orbits in the circular restricted three-body problem with the more massive primary as an oblate spheroid
2020
[9] Halo Orbits in the Photo-Gravitational Restricted Three-Body Problem
2019
[10] Searching for g modes
2019
[11] Natural formation flying on quasi-halo orbits in the photogravitational circular restricted three-body problem
Acta Astronautica, 2018
[12] Dynamics of the spatial restricted three-body problem stabilized by Hamiltonian structure-preserving control
Nonlinear Dynamics, 2018
[13] Searching for g modes: Part I. A new calibration of the GOLF instrument
2018
[14] Searching for g modes-I. A new calibration of the GOLF instrument
2018
[15] Oblateness Effect of Saturn on Halo Orbits of L1 and L2 in Saturn-Satellites Restricted Three-Body Problem
2016
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