非自主扁圆形地月系统的太阳帆轨道运动:周期轨道家族

IF 2.2 3区 工程技术 Q2 MECHANICS
Ehsan Abbasali, Amirreza Kosari, Majid Bakhtiari
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引用次数: 0

摘要

本文的主要目的是在扁球形地月圆形受限三体问题(CR3BP)中确定太阳帆的周期轨道。将太阳加速度纳入地月系统会修改轨道方程,将传统的 CR3BP 从自主系统转变为非自主系统。因此,识别周期轨道的程序与传统的自主 CR3BP 方法不同。因此,本文介绍了一种在非自主 CR3BP 中识别新周期 Halo 和 Lyapunov 轨道的新方法。我们提出的方法包括四个分层步骤:首先,进行截面模拟(Poincaré 地图),以获得自主 CR3BP 内轨道状态向量的初始近似值。其次,利用自主 CR3BP 方程开发周期性轨道修正算法,以获得精确的初始条件。第三步,将自主 CR3BP 周期轨道的初始条件作为周期轨道修正算法的输入,得出太阳帆周期轨道的初始条件。在最后一步,通过逐渐增加风帆的特征加速度来生成一系列轨道。我们的工作解决了以往研究的局限性,以往的研究仅依赖于早期研究中报告的无扰动自主 CR3BP 得出的初始猜测,这往往会导致非自主系统中遗漏大量太阳帆周期轨道。这种方法能够在地月系统中发现新的周期轨道,并考虑到来自扁圆主星的扰动,包括从\({j}_{2}\)到\({j}_{6}\)的带状谐波项。通过模拟太阳帆 Lyapunov 和 Halo 轨道验证了这一方法,从而提供了对非自主条件下地月 CR3BP 的全面理解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Solar sail orbital motion at the non-autonomous oblate earth-moon system: family of periodic orbits

Solar sail orbital motion at the non-autonomous oblate earth-moon system: family of periodic orbits

The primary objective of this paper is to identify periodic orbits for solar sails within the oblate Earth-Moon Circular Restricted Three-Body Problem (CR3BP). Incorporating solar acceleration into the Earth-Moon system modifies the governing orbital equations, transforming the traditional CR3BP from an autonomous to a non-autonomous system. As a result, the procedure for identifying periodic orbits diverges from the conventional autonomous CR3BP method. Thus, this paper introduces a novel methodology to identify new periodic Halo and Lyapunov orbits within the non-autonomous CR3BP. Our proposed approach comprises four hierarchical steps: first, a surface of section simulation (Poincaré map) is conducted to obtain an initial approximation of the orbital state vector within the autonomous CR3BP. Second, a periodic orbit correction algorithm is developed using the autonomous CR3BP equations to acquire precise initial conditions. In the third step, initial conditions for solar sail periodic orbits are derived by applying the initial conditions of autonomous CR3BP periodic orbits as inputs to the periodic orbit correction algorithm, which is now executed using non-autonomous CR3BP equations. In the final step, a family of orbits is generated by gradually increasing the sail's characteristic acceleration. Our work addresses limitations in previous studies that relied on initial guesses derived solely from the unperturbed autonomous CR3BP reported in earlier research, which often resulted in the missing of numerous solar sail periodic orbits in the non-autonomous system. This approach enables the discovery of new periodic orbits within the Earth-Moon system, accounting for perturbations from the oblate primaries, including zonal harmonic terms from \({j}_{2}\) to \({j}_{6}\). The methodology is validated through simulations of solar sail Lyapunov and Halo orbits, offering a comprehensive understanding of the Earth-Moon CR3BP under non-autonomous conditions.

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来源期刊
CiteScore
4.40
自引率
10.70%
发文量
234
审稿时长
4-8 weeks
期刊介绍: Archive of Applied Mechanics serves as a platform to communicate original research of scholarly value in all branches of theoretical and applied mechanics, i.e., in solid and fluid mechanics, dynamics and vibrations. It focuses on continuum mechanics in general, structural mechanics, biomechanics, micro- and nano-mechanics as well as hydrodynamics. In particular, the following topics are emphasised: thermodynamics of materials, material modeling, multi-physics, mechanical properties of materials, homogenisation, phase transitions, fracture and damage mechanics, vibration, wave propagation experimental mechanics as well as machine learning techniques in the context of applied mechanics.
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