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Design of Neural Networks for Fast Convergence and Accuracy

机译:快速收敛和精度的神经网络设计

摘要

A novel procedure for the design and training of artificial neural networks, used for rapid and efficient controls and dynamics design and analysis for flexible space systems, has been developed. Artificial neural networks are employed to provide a means of evaluating the impact of design changes rapidly. Specifically, two-layer feedforward neural networks are designed to approximate the functional relationship between the component spacecraft design changes and measures of its performance. A training algorithm, based on statistical sampling theory, is presented, which guarantees that the trained networks provide a designer-specified degree of accuracy in mapping the functional relationship. Within each iteration of this statistical-based algorithm, a sequential design algorithm is used for the design and training of the feedforward network to provide rapid convergence to the network goals. Here, at each sequence a new network is trained to minimize the error of previous network. The design algorithm attempts to avoid the local minima phenomenon that hampers the traditional network training. A numerical example is performed on a spacecraft application in order to demonstrate the feasibility of the proposed approach.
机译:已经开发了一种用于设计和训练人工神经网络的新颖程序,用于快速有效的控制以及柔性空间系统的动力学设计和分析。人工神经网络被用来提供一种评估设计变更影响的方法。具体来说,设计了两层前馈神经网络,以近似组成航天器设计变化与其性能度量之间的功能关系。提出了一种基于统计采样理论的训练算法,该算法保证了训练后的网络在映射功能关系时提供了设计人员指定的准确性。在这种基于统计的算法的每次迭代中,将顺序设计算法用于前馈网络的设计和训练,以快速收敛到网络目标。在这里,在每个序列上,都会训练一个新的网络以最小化先前网络的错误。该设计算法试图避免妨碍传统网络训练的局部极小现象。为了证明该方法的可行性,在航天器应用上进行了数值算例。

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