11   Artículos

 
en línea
Shuai Zheng, Yumin Su, Jiayuan Zhuang, Yueqi Tang and Guangjie Yi    
The development of dynamic positioning (DP) algorithms for an unmanned surface vehicle (USV) is attracting great interest, especially in support of complex missions such as sea rescue. In order to improve the simplicity of the algorithm, a DP algorithm b... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Chen Xu, Yang Wang, Zhiqi Niu, Sheng Luo and Fenghuai Du    
In this paper, by accounting for the angle constraint (AC) and autopilot lag compensation (ALC), a novel fixed-time convergent guidance law is developed based on a fixed-time state observer and bi-limit homogeneous technique. The newly proposed guidance ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Ting Wang and Heng Shi    
A fixed-time nonlinear circular guidance law that satisfies the impact time constraint is proposed. By utilizing the geometric principle that the length of a circular arc connecting the missile and the target can be analytically calculated, the exact exp... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mingkun Guo, Guangqing Xia, Feng Yang, Cong Liu, Kai Liu and Jingnan Yang    
This paper studies a cooperative encirclement interception guidance law against a maneuvering target that utilizes a leader?follower control scheme. The control design is decoupled into two parts. In the line-of-sight (LOS) direction, a fixed-time distri... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Simone Battistini, Giulio De Angelis, Mauro Pontani and Filippo Graziani    
Modern space missions often require satellites to perform guidance, navigation, and control tasks autonomously. Despite their limited resources, small satellites are also involved in this trend, as in-orbit rendezvous and docking maneuvers and formation ... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Xiaoma Liu, Yang Han, Peng Li, Hongwu Guo and Wenqi Wu    
The problem that two cooperative missiles intercept a maneuvering target while imposing a desired relative geometry is investigated in the paper. Firstly, a three-dimensional (3D) estimation model for cooperative target tracking is proposed and the obser... ver más
Revista: Aerospace    Formato: Electrónico

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