Trajectory Design for L2 Halo Orbits in the Sun-Earth System: Utilizing Invariant Manifolds with Radiation Pressure and Oblateness Effects

Trajectory Design for L2 Halo Orbits in the Sun-Earth System: Utilizing Invariant Manifolds with Radiation Pressure and Oblateness Effects

Item #:: 080560-0021
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DOI: https://doi.org/10.52202/080560-0021
Author(s): Abhistha Singh, Jai Kumar
Pages: 158-172 (15 pages)
Format: PDF Paper Download
Conference: Navigation, Guidance and Control for Deep Space Missions
Date/Location: Held 7-9 May 2025, New Delhi, India.
Publisher: International Astronautical Federation (IAF)

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DOI: https://doi.org/10.52202/080560-0021
Author(s): Abhistha Singh, Jai Kumar
Pages: 158-172 (15 pages)
Format: PDF Paper Download
Conference: Navigation, Guidance and Control for Deep Space Missions
Date/Location: Held 7-9 May 2025, New Delhi, India.
Publisher: International Astronautical Federation (IAF)