[1] Y. Tsuda and et al., “Achievement of IKAROS—Japanese deep space solar sail demonstration mission,” Acta Astronaut., vol. 82, no. 2, pp. 183–188, 2013.
[2] J. Lievre, “Solar sailing attitude control of large geostationary satellite,” in Automatic Control in Space 1985, Elsevier, pp. 29–32,1986.
[3] A. Colagrossi and M. Lavagna, “Preliminary results on the dynamics of large and flexible space structures in Halo orbits,” Acta Astronaut., vol. 134, pp. 355–367, 2017, doi: https://doi.org/10.1016/j.actaastro.2017.02.020.
[4] M. Xu and S. Xu, “Structure-Preserving Stabilization for Hamiltonian System and its Applications in Solar Sail,” J. Guid. Control. Dyn., vol. 32, no. 3, pp. 997–1004, May 2009, doi: 10.2514/1.34757.
[5] H. D. Curtis, Orbital mechanics for engineering students. Butterworth-Heinemann, 2013.
[6] K. I. Alvarado and S. K. Singh, “Orbit maintenance via homeomorphic, periodic orbit revs in the Elliptic Restricted Three-Body Problem,” in Proceedings of the 2023 AAS/AIAA Astrodynamics Specialist Conference, Big Sky, MT, USA, pp. 13–17,2023.
[7] V. Y. Kezerashvili and R. Y. Kezerashvili, “Theoretical approach to circular solar sail deployment,” Adv. Sp. Res., vol. 73, no. 9, pp. 4731–4741, 2024.
[8] E. Abbasali and M. Bakhteiari, “Restricted three body problem considering the perturbations of both oblate massive primaries,” J. Aerosp. Sci. Technol., vol. 13, no. 2.
[9] A. Soumakh, K. Raeisi, O. Negarash, and M. Navabi, “Orbital altitude increase maneuver using an ideal solar sail up to the L1 Lagrange point for a Galileo satellite located in MEO orbit,” presented at the International Conference of the Iranian Aerospace Society, 2014.
[10] M.-H. Salehnia, J. Shirazi, and R. Esmailzadeh, “Attitude control of an Earth-pointing satellite using solar panels without azimuth angle and gyroscope measurements,” presented at the International Conference of the Iranian Aerospace Society, 2013.
[11] E. Abbasali, A. Kosari, and M. Bakhtiari, “Effects of oblateness of the primaries on natural periodic orbit-attitude behaviour of satellites in three body problem,” Adv. Sp. Res., 2021.
[12] E. I. Abouelmagd, A. A. Alshaery, and F. Gao, “New dynamical system for circular satellites relative motion,” Chaos, Solitons & Fractals, vol. 182, p. 114879, 2024.
[13] M. Bakhtiari, E. Abbasali, and K. Daneshjoo, “Minimum Cost Perturbed Multi-impulsive Maneuver Methodology to Accomplish an Optimal Deployment Scheduling for a Satellite Constellation,” J. Astronaut. Sci., vol. 70, no. 3, p. 18, 2023.
[14] D. Lichodziejewski, B. Derbes, K. Slade, and T. Mann, “Vacuum deployment and testing of a 4-quadrant scalable inflatable rigidizable solar sail system,” in 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2005, p. 2122.
[15] J. ACORD and J. Nicklas, “Theoretical and Practical Aspects of Solar Pressure Attitude Controlfor Interplanetary Spacecraft,” in Guidance and Control Conference, 1964, p. 327.
[16] P. Musen, “The influence of the solar radiation pressure on the motion of an artificial satellite,” J. Geophys. Res., vol. 65, no. 5, pp. 1391–1396, 1960.
[17] K. C. Howell, “Three-dimensional, periodic,‘halo’orbits,” Celest. Mech., vol. 32, no. 1, pp. 53–71, 1984.
[18] V. K. Srivastava, J. Kumar, and B. S. Kushvah, “Regularization of circular restricted three-body problem accounting radiation pressure and oblateness,” Astrophys. Space Sci., vol. 362, no. 3, p. 49, 2017.