Balancing Conditions for the Relativistic Correction Using Lorentz Acceleration

In this work, the average effects of the Lorentz acceleration on the charged spacecraft’s orbit are studied encounter with relativistic correction. The relativistic correction as function of the orbital elements, and may be time, is formulated. Lagrange planetary equations are used to calculate the...

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Hlavní autoři: M. A. Yousef, M. I. El-Saftawy, A. Mostafa
Médium: Článek
Jazyk:English
Vydáno: Hindawi Limited 2023-01-01
Edice:International Journal of Aerospace Engineering
On-line přístup:http://dx.doi.org/10.1155/2023/5593887