4   Artículos

 
en línea
Ali Raza and Hua Wang    
This paper presents a two-phase guidance and control algorithm to extend the range and improve the impact point accuracy of a 122-mm rocket using a fixed canards trajectory correction fuze. The guidance algorithm consists of a unique glide and correction... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhiwei Yang, Liangming Wang and Jianwei Chen    
In this paper, a new dual-spin guided projectile that is equipped with ten lateral impulse jets is proposed for trajectory correction. To guide the overall design of the projectile and the control system, a linear motion model of the projectile that was ... ver más
Revista: Aerospace    Formato: Electrónico

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