通过量子退火的行星际轨迹的转录和优化

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Federico De Grossi, Andrea Carbone, Dario Spiller, Daniele Ottaviani, Riccardo Mengoni, Christian Circi
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引用次数: 0

摘要

本文采用量子退火框架求解航天器轨道优化问题。量子退火属于量子计算领域,是一种很有前途的利用量子退火炉来解决硬二进制优化问题的技术。为了利用量子退火解决轨迹的最优控制问题,引入了一个转录过程,将问题表示为所需的二进制优化形式。该方法利用伪谱方法对轨迹进行离散化,并将动力学约束表示为特定节点上的代数等式约束。在此基础上,给出了该问题实值变量的线性化过程和二值化表示策略,得到了二次型二值无约束优化形式。基于量子退火的方法在从地球到火星的行星际低推力转移的背景下进行了测试。首先,我们讨论了问题的哪些实例,特别是就其维度而言,可以在当前可用的量子退火炉上实现;然后,通过使用D-Wave系统的退火炉来寻求解决方案。探索了经典与量子资源相结合的混合求解器和全量子求解器的解。结果证明了转录方法的有效性,证明了混合求解器解决案例研究问题的能力,并突出了量子退火实际轨迹优化的有前途的特征和当前的局限性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Transcription and optimization of an interplanetary trajectory through quantum annealing

This study employed a quantum-annealing framework to solve spacecraft trajectory optimization problems. Quantum annealing belongs to the field of quantum computing and is a promising technique for tackling hard binary optimization problems by employing quantum annealers. To address the optimal control of a trajectory using quantum annealing, a transcription procedure was introduced to express the problem in the binary optimization form required. The proposed procedure leverages the pseudospectral method to discretize the trajectory and represents the dynamical constraints as algebraic equality constraints at specific nodes. Subsequently, both a linearization procedure and binary representation strategy for the real-valued variables of the problem were presented, leading to the quadratic binary unconstrained optimization form. The quantum-annealing-based method was tested in the context of an interplanetary low-thrust transfer from the Earth to Mars. First, we discussed which instances of the problem, especially in terms of their dimensions, are implementable on currently available quantum annealers; then, a solution was sought by employing annealers from D-Wave systems. Solutions from hybrid solvers that combine classical and quantum resources, and fully quantum solvers were explored. The results demonstrate the validity of the transcription approach, demonstrate the ability of the hybrid solver to tackle the case-study problem, and highlight the promising features and current limitations of practical trajectory optimization with quantum annealing.

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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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