Abstract
A key challenge in low-thrust trajectory design is generating preliminary solutions that simultaneously specify the spacecraft position and velocity vectors, as well as the thrust history. To mitigate this difficulty, dynamical structures within a combined low-thrust circular restricted 3-body problem (CR3BP) are investigated as candidate solutions to seed initial low-thrust trajectory designs. The addition of a low-thrust force to the CR3BP modifies the locations and stability of the equilibria, offering novel geometries for mission applications. Transfers between these novel equilibria are constructed by leveraging the associated stable and unstable manifolds and insights from the low-thrust CR3BP.
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Acknowledgements
The authors thank the Purdue University School of Aeronautics and Astronautics for the facilities and support, including access to the Rune and Barbara Eliasen Visualization Laboratory. Additionally, many thanks to the Purdue Multi-Body Dynamics Research Group, the JPL Mission Design and Navigation branch, and Dr. Dan Grebow for interesting discussions and ideas. This research is supported by a National Aeronautics and Space Administration (NASA) Space Technology Research Fellowship, NASA Grant NNX16AM40H. The authors are grateful to the reviewers for providing thorough and insightful feedback on this paper; it has certainly been improved as a result.
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The original version of this paper was presented during the AAS/AIAA Astrodynamics Specialist Conference in Snowbird, Utah in August 2018. This work is supported by a NASA Space Technology Research Fellowship, NASA Grant NNX16AM40H
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Cox, A.D., Howell, K.C. & Folta, D.C. Trajectory Design Leveraging Low-Thrust, Multi-Body Equilibria and their Manifolds. J Astronaut Sci 67, 977–1001 (2020). https://doi.org/10.1007/s40295-020-00211-6
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DOI: https://doi.org/10.1007/s40295-020-00211-6