Analysis of the Effects of Electromagnetic Forces on the Relative Motion of a Charged Spacecraft Formation Flying

IF 0.7 Q4 ASTRONOMY & ASTROPHYSICS
S. Tealib, Y. Abdel-Aziz, M. E. Awad, K. Khalil, M. Radwan
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引用次数: 0

Abstract

Abstract In recent years, studying Lorentz’s force has become a possible good means to control the spacecraft to reduce the fuel cost by modulating spacecraft electrostatic charge (magnetic and electric fields). The generation of Lorentz force is finite by the natural magnetic field and the relative velocity of the spacecraft. Therefore, the Lorentz force cannot fully occur from conventional propulsion technologies. Previous studies are concerned with studying Lorentz’s strength in the magnetic field only. In this work, we developed a mathematical model for a new technique establishing a raise in the level of charging in the spacecraft surface that is moving in the Earth’s magnetic field and provided by modulating spacecraft’s electrostatic charge that induces acceleration via the Lorentz force. The acceleration will be used to find the relationship between capacitance and power required to minimize the consumption of control energy used in such cases or to replace the usual control thruster by Lorentz force.
电磁力对带电航天器编队相对运动影响的分析
摘要近年来,研究洛伦兹力已成为通过调节航天器静电荷(磁场和电场)来控制航天器以降低燃料成本的一种可能的好方法。洛伦兹力的产生受到自然磁场和航天器相对速度的限制。因此,洛伦兹力不能完全由传统的推进技术产生。以前的研究只关注研究洛伦兹在磁场中的强度。在这项工作中,我们为一种新技术开发了一个数学模型,该技术通过调制航天器的静电荷来提高在地球磁场中移动的航天器表面的电荷水平,该静电荷通过洛伦兹力感应加速度。加速度将用于找到电容和功率之间的关系,以最大限度地减少在这种情况下使用的控制能量的消耗,或者用洛伦兹力代替通常的控制推进器。
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CiteScore
1.00
自引率
11.10%
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0
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