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

Author:

Zhang Xue1,Hong Haichao1ORCID

Affiliation:

1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China

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.

Funder

National defense foundation strengthening funds

Frontier science and technology innovation fund

Publisher

MDPI AG

Reference29 articles.

1. Optimal three-dimensional impact time guidance with seeker’s field-of-view constraint;He;Chin. J. Aeronaut.,2021

2. Cooperative motion planning and control for aerial-ground autonomous systems: Methods and applications;Chai;Prog. Aerosp. Sci.,2024

3. Equinoctial Lyapunov control law for low-thrust rendezvous;Narayanaswamy;J. Guid. Control Dyn.,2023

4. Robust spacecraft guidance around small bodies under uncertainty: Stochastic optimal control approach;Oguri;J. Guid. Control Dyn.,2021

5. Peterson, J.T., Singh, S.K., Junkins, J.L., and Taheri, E. (February, January 30). Lyapunov guidance in orbit element space for low-thrust cislunar trajectories. Proceedings of the AAS Guidance, Navigation and Control, Breckenridge, CO, USA.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3