利用洛伦兹加速度进行相对论性修正的平衡条件

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
M. A. Yousef, M. El-Saftawy, A. Mostafa
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引用次数: 0

摘要

本文研究了洛伦兹加速度对带电航天器轨道的平均影响,并进行了相对论修正。相对论修正是轨道元素的函数,可能是时间,公式化了。拉格朗日行星方程用于计算由于所考虑的扰动力引起的扰动。导出了利用洛伦兹加速度抵消相对论修正效应所需的条件。应用了不同轨道类型的数值例子。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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 perturbations due to considered perturbing forces. The needed conditions to neutralize the effects of the relativistic corrections, using Lorentz acceleration, are derived. Numerical examples for different kinds of orbits are applied.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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