Enhanced Computational Biased Proportional Navigation with Neural Networks for Impact Time Control

Advanced computational methods are being applied to address traditional guidance problems, yet research is still ongoing regarding how to utilize them effectively and scientifically. A numerical root-finding method was proposed to determine the bias in biased proportional navigation to achieve the impact time control without time-to-go estimation. However, the root-finding algorithm in the original method might experience efficiency and convergence issues. This paper introduces an enhanced method based on neural networks, where the bias is directly output by the neural networks, significantly improving computational efficiency and addressing convergence issues. The novelty of this method lies in the development of a reasonable structure that appropriately integrates off-the-shelf machine learning techniques to effectively enhance the original iteration-based methods. In addition to demonstrating its effectiveness and performance of its own, two comparative scenarios are presented: (a) Evaluate the time consumption when both the proposed and the original methods operate at the same update frequency. (b) Compare the achievable update frequencies of both methods under the condition of equal real-world time usage.

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Publication Details

Journal
Aerospace
Published
2024-08-15
DOI
https://doi.org/10.3390/aerospace11080670
Citations
2
Primary Topic
Guidance and Control Systems
Type
article
Field-Weighted Citation Impact
2.60
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article

Enhanced Computational Biased Proportional Navigation with Neural Networks for Impact Time Control

Haichao Hong, Xue Zhang
2 citations
Aerospace
Guidance and Control Systems
2.60
article

Enhanced Computational Biased Proportional Navigation with Neural Networks for Impact Time Control

Haichao Hong, Xue Zhang
article en
2 citations

Abstract

Advanced computational methods are being applied to address traditional guidance problems, yet research is still ongoing regarding how to utilize them effectively and scientifically. A numerical root-finding method was proposed to determine the bias in biased proportional navigation to achieve the impact time control without time-to-go estimation. However, the root-finding algorithm in the original method might experience efficiency and convergence issues. This paper introduces an enhanced method based on neural networks, where the bias is directly output by the neural networks, significantly improving computational efficiency and addressing convergence issues. The novelty of this method lies in the development of a reasonable structure that appropriately integrates off-the-shelf machine learning techniques to effectively enhance the original iteration-based methods. In addition to demonstrating its effectiveness and performance of its own, two comparative scenarios are presented: (a) Evaluate the time consumption when both the proposed and the original methods operate at the same update frequency. (b) Compare the achievable update frequencies of both methods under the condition of equal real-world time usage.

AerospaceVol. 11(8)
Shanghai Jiao Tong University (CN)
Affordable and clean energy
Openalex Percentile: Top 9%
Guidance and Control Systems
2.60
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Enhanced Computational Biased Proportional Navigation with Neural Networks for Impact Time Control — Haichao Hong, Xue Zhang · Aerospace (2024) | TGRS Research Map | TGRS