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• W4280494595 abstract "Abstract This study made use of a shape-based method to analyze the orbital dynamics of a spacecraft subject to a continuous propulsive acceleration acting along the circumferential direction. Under the assumption of a logarithmic spiral trajectory, an exact solution to the equations of motion exists, which allows the spacecraft state variables and flight time to be expressed as a function of the angular coordinate. There is also a case characterized by specific initial conditions in which the time evolution of the state variables may be analytically determined. In this context, the presented solution is used to analyze circle-to-circle trajectories, where the combination of two impulsive maneuvers and a logarithmic spiral path are used to accomplish the transfer. The determined results are then applied to the achievement of the Earth—Mars and the Earth—Venus transfers using actual data from a recent thruster developed by NASA." @default.
• W4280494595 created "2022-05-22" @default.
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• W4280494595 date "2022-05-18" @default.
• W4280494595 modified "2023-09-26" @default.
• W4280494595 title "Analytical solution to logarithmic spiral trajectories with circumferential thrust and mission applications" @default.
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• W4280494595 doi "https://doi.org/10.1007/s42064-022-0135-3" @default.
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