4.3 Article

A deep learning-based approach to time-coordination entry guidance for multiple hypersonic vehicles

期刊

AERONAUTICAL JOURNAL
卷 -, 期 -, 页码 -

出版社

CAMBRIDGE UNIV PRESS
DOI: 10.1017/aer.2022.82

关键词

Hypersonic glide vehicles; Cooperative entry guidance; Neural network; Deep learning; Extended Kalman filter

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This study proposes a multiple-vehicles time-coordination guidance technique based on deep learning to tackle the cooperative guiding problem of hypersonic gliding vehicle entry phase. A dual-parameter bank angle profile is utilized for longitudinal guiding, supported by a vehicle trajectory database and a deep neural network (DNN) structure. An extended Kalman filter is also constructed for real-time detection of changes in aerodynamic parameters, which are fed into the DNN. The lateral guiding adopts a logic based on the segmented heading angle error corridor. The results show that the built DNN effectively addresses the cooperative guiding requirements with high accuracy, fast response time, and ability to handle disruptions in aerodynamic parameters without inter-munition communication.
A multiple-vehicles time-coordination guidance technique based on deep learning is suggested to address the cooperative guiding problem of hypersonic gliding vehicle entry phase. A dual-parameter bank angle profile is used in longitudinal guiding to meet the requirements of time coordination. A vehicle trajectory database is constructed along with a deep neural network (DNN) structure devised to fulfill the error criteria, and a trained network is used to replace the conventional prediction approach. Moreover, an extended Kalman filter is constructed to detect changes in aerodynamic parameters in real time, and the aerodynamic parameters are fed into a DNN. The lateral guiding employs a logic for reversing the sign of bank angle, which is based on the segmented heading angle error corridor. The final simulation results demonstrate that the built DNN is capable of addressing the cooperative guiding requirements. The algorithm is highly accurate in terms of guiding, has a fast response time, and does not need inter-munition communication, and it is capable of solving guidance orders that satisfy flight requirements even when aerodynamic parameter disruptions occur.

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