20   Artículos

 
en línea
Hyeong-Geun Kim and Jongho Shin    
This paper proposes an impact time control guidance law based on exact nonlinear kinematics equations. To address the impact time control problem of providing enhanced intercept accuracy, we formulated an error variable whose regulation ensures the fulfi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ce Zhang, Duanyang Geng, Haigang Xu, Xinao Li, Jiarui Ming, Duanxin Li and Qihuan Wang    
The air distribution and speed uniformity of the cleaning fan in the cleaning room have a great influence on the working quality of the cleaning system of the harvester. In view of the problem of uneven air distribution in the cleaning room caused by imp... ver más
Revista: Agriculture    Formato: Electrónico

 
en línea
Wei Jiang, Yongxi Lyu and Jingping Shi    
This paper proposes an approach of target tracking of a ground target for UAVs using Optimal Two-Stage Cubature Kalman Filter and Improved Coordinated Lateral Guidance Law. Firstly, the Optimal Two-Stage Cubature Kalman Filter (OTSCKF) is proposed to est... ver más
Revista: ISPRS International Journal of Geo-Information    Formato: Electrónico

 
en línea
Yifan Deng, Jinlei Ren, Xu Wang and Yuanli Cai    
To address the need for flexible energy management and impact angle control in the midcourse guidance of modern long-range antiballistic interceptors, an impact time and angle guidance law is designed for the exoatmospheric midcourse flight of antiballis... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chendi Li, Jiang Wang and Peng Huang    
This correspondence proposes an optimal cooperative guidance law for protecting a target from a guided missile. The linearized three-body kinematics using the line-of-sight (LOS) triangle concept is formulated, and a new concept called error distance is ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Wanqing Zhang, Wanchun Chen and Wenbin Yu    
A new, highly constrained guidance law is proposed against a maneuvering target while satisfying both impact angle and terminal acceleration constraints. Here, the impact angle constraint is addressed by solving an optimal guidance problem in which the t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yingkai Xia, Zhemin Huang, Kan Xu, Guohua Xu and Ye Li    
This paper proposes a novel three-dimensional trajectory tracking control methodology for a heterogeneous X-rudder autonomous underwater vehicle (XAUV) that can achieve finite-time convergence, complex actuator dynamics handling, and energy-efficient opt... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Sijia Tao, Guangtai Shi, Yexiang Xiao, Zongliu Huang and Haigang Wen    
When the multiphase pump is running, the internal medium often exists as bubble flow. In order to investigate the bubble occurrence characteristics in the pressurization unit of the multiphase pump more accurately, this paper couples computational fluid ... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Shilei Zhao, Wanchun Chen and Liang Yang    
This paper aims to develop an optimal guidance law for exo-atmospheric interception, in which impact-angle constraint and acceleration limit are considered. Firstly, an optimal control problem with constraints on terminal miss and impact-angle is formula... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Hyeong-Geun Kim and Jun-Yong Lee    
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow field-of-view of the seekers. As groundwork for designing a guidance law, we first present a general guidance structure that can achieve any terminal const... ver más
Revista: Aerospace    Formato: Electrónico

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