Ensemble Transfer Learning Midcourse Guidance Algorithm for Velocity Maximization

被引:2
|
作者
Jin, Tianyu [1 ]
He, Shaoming [1 ,2 ]
机构
[1] Beijing Inst Technol, Beijing 100081, Peoples R China
[2] Sch Aerosp Engn, 5th Zhongguancun South St, Beijing, Peoples R China
来源
关键词
Missile Guidance and Control; Generative Adversarial Network; Guidance and Navigational Algorithms; Terminal Velocity; Flight Path Angle; Aerodynamic Coefficients; Biased Proportional Navigation Guidance; Optimal Control Theory; Aerodynamic Performance; NETWORKS;
D O I
10.2514/1.I011070
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes an ensemble transfer learning guidance algorithm for angular-constrained midcourse guidance to maximize the terminal velocity. The algorithm developed improves the generalization capability of the trained deep neural network to adapt to a new environment. First several deep neural guidance networks are trained for some specific working environments via supervised learning. A small-scale ensemble transfer learning network is then leveraged to fuse the knowledge of different pretrained deep neural network. This requires much less labeled data to transfer existing knowledge to a new working environment and hence greatly improves the learning efficiency, compared to the supervised learning philosophy. Extensive numerical simulations are performed to demonstrate the effectiveness of the proposed algorithm.
引用
收藏
页码:204 / 215
页数:12
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