Artificial Intelligence Based Spacecraft Resilience Optimization in Space Informatics Digital Twins

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2024-09-12 DOI:10.1109/TAES.2024.3459879
Zhihan Lyu;Jinkang Guo;Ranran Lou;Haibin Lv
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Abstract

This article focuses on optimizing the elasticity of spacecraft by harnessing the power of artificial intelligence (AI) technology. With the support of spatial informatics and digital twins technology, this work initially employs AI techniques, specifically the radial basis function neural networks, a deep learning algorithm, to perform global optimization and orbit fitting for spacecraft. Augmented Lagrangian multipliers are then introduced to locally optimize this neural network. Additionally, to further enhance the spacecraft's flexibility, an improved particle swarm optimization (PSO) algorithm is applied to optimize the proposed network. The work also introduces a periodic variational multiobjective quantum particle swarm optimization (PMQPSO) algorithm. Subsequently, a rigid-flexible coupled dynamics model for the spacecraft is established, and relevant simulations and experiments are conducted to support this work. The results indicate that the average fitness of the improved PMQPSO algorithm decreases to 18.23 after 500 iterations, with its performance being at least 3.2% higher than that of the classical quantum PSO algorithm. Furthermore, after the initial decline in the first order, the limiter residuals no longer decline and exhibit convergence, as the residual curve transitions from high to low, indicating a gradual improvement in convergence and stability. These findings highlight the advantages of the PMQPSO algorithm in optimizing the spacecraft's elasticity. In conclusion, this parameter optimization holds practical significance for the design optimization of aircraft aerodynamic shapes.
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空间信息学数字双胞胎中基于人工智能的航天器弹性优化
本文的重点是利用人工智能(AI)技术的力量来优化航天器的弹性。在空间信息学和数字孪生技术的支持下,本工作初步采用人工智能技术,特别是径向基函数神经网络,一种深度学习算法,对航天器进行全局优化和轨道拟合。然后引入增广拉格朗日乘子对神经网络进行局部优化。此外,为了进一步提高航天器的灵活性,采用改进的粒子群优化算法(PSO)对网络进行优化。本文还介绍了一种周期变分多目标量子粒子群优化算法。随后,建立了航天器刚柔耦合动力学模型,并进行了相应的仿真和实验支持。结果表明,经过500次迭代后,改进PMQPSO算法的平均适应度降至18.23,性能比经典量子PSO算法提高至少3.2%。此外,残差曲线在初始一阶下降后,极限残差不再下降,呈现收敛性,残差曲线由高向低过渡,表明收敛性和稳定性逐渐提高。这些发现突出了PMQPSO算法在优化航天器弹性方面的优势。综上所述,该参数优化对于飞机气动外形的设计优化具有实际意义。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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