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An analytical expresssion of the polar form of the trajectory equation of a spacecraft propelled by a zero-pitch angle electric solar wind sail (E-sail) does not exist. Using homotopy perturbation technique, an approximate form of such a polar equation is obtained, both for the circular and the weakly-elliptical parking orbit cases.

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This page is a summary of: Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation Technique, Journal of Guidance Control and Dynamics, April 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g007219.
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