12   Artículos

 
en línea
Yunhe Guo, Zijian Jiang, Hanqiao Huang, Hongjia Fan and Weiye Weng    
In order to improve the problem of overly relying on situational information, high computational power requirements, and weak adaptability of traditional maneuver methods used by hypersonic vehicles (HV), an intelligent maneuver strategy combining deep r... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mengjing Gao, Tian Yan, Quancheng Li, Wenxing Fu and Jin Zhang    
As defense technology develops, it is essential to study the pursuit?evasion (PE) game problem in hypersonic vehicles, especially in the situation where a head-on scenario is created. Under a head-on situation, the hypersonic vehicle?s speed advantage is... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Haizhao Liang, Zhi Li, Jinze Wu, Yu Zheng, Hongyu Chu and Jianying Wang    
The guidance problem of a confrontation between an interceptor, a hypersonic vehicle, and an active defender is investigated in this paper. As a hypersonic multiplayer pursuit-evasion game, the optimal guidance scheme for each adversary in the engagement... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Bin Yang, Pengxuan Liu, Jinglang Feng and Shuang Li    
This paper presents a novel and robust two-stage pursuit strategy for the incomplete-information impulsive space pursuit-evasion missions considering the J2 perturbation. The strategy firstly models the impulsive pursuit-evasion game problem into a far-d... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ziwen Wang, Baichun Gong, Yanhua Yuan and Xin Ding    
Aiming to solve the optimal control problem for the pursuit-evasion game with a space non-cooperative target under the condition of incomplete information, a new method degenerating the game into a strong tracking problem is proposed, where the unknown t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Junfeng Zhou, Lin Zhao, Jianhua Cheng, Shuo Wang and Yipeng Wang    
This paper studies the orbital pursuit-evasion-defense problem with the continuous low thrust propulsion. A control strategy for the pursuer is proposed based on the fuzzy comprehensive evaluation and the differential game. First, the system is described... ver más
Revista: Applied Sciences    Formato: Electrónico

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