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Improved magnetic charged system search optimization algorithm with application to satellite formation flying

机译:改进的带电系统搜索优化算法及其在卫星编队飞行中的应用

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摘要

This paper is devoted to the implementation and application of an improved version of the metaheuristic algorithm called magnetic charged system search. Some modifications and novelties are introduced and tested. Firstly, the authors' attempt is to develop a self-adaptive and user-friendly algorithm which can automatically set all the preliminary parameters (such as the numbers of particles, the maximum iterations number) and the internal coefficients. Indeed, some mathematical laws are proposed to set the parameters and many coefficients can dynamically change during the optimization process based on the verification of internal conditions. Secondly, some strategies are suggested to enhance the performances of the proposed algorithm. A chaotic local search is introduced to improve the global best particle of each iteration by exploiting the features of ergodicity and randomness. Moreover, a novel technique is proposed to handle bad-defined boundaries; in fact, the possibility to self-enlarge the boundaries of the optimization variables is considered, allowing to achieve the global optimum even if it is located on the boundaries or outside. The algorithm is tested through some benchmark functions and engineering design problems, showing good results, followed by an application regarding the problem of time-suboptimal manoeuvres for satellite formation flying, where the inverse dynamics technique, together with the B-splines, is employed. This analysis proves the ability of the proposed algorithm to optimize control problems related to space engineering, obtaining better results with respect to more common and used algorithms in literature.
机译:本文致力于实现和应用一种改进的改进的启发式算法,称为磁带电系统搜索。引入了一些修改和新颖性并进行了测试。首先,作者的尝试是开发一种自适应且用户友好的算法,该算法可以自动设置所有初步参数(例如粒子数,最大迭代数)和内部系数。实际上,已经提出了一些数学定律来设置参数,并且基于内部条件的验证,在优化过程中许多系数可以动态变化。其次,提出了一些提高算法性能的策略。通过利用遍历性和随机性的特征,引入了混沌局部搜索来改善每次迭代的全局最佳粒子。此外,提出了一种新技术来处理定义不明确的边界。实际上,考虑了自动扩大优化变量边界的可能性,即使全局最优位于边界或外部也可以实现。该算法通过一些基准函数和工程设计问题进行了测试,显示出了良好的效果,随后针对卫星编队飞行的时间次优操纵问题进行了应用,其中采用了逆动力学技术以及B样条。该分析证明了该算法具有优化与空间工程相关的控制问题的能力,相对于文献中更为常见和使用的算法,可以获得更好的结果。

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