4   Artículos

 
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
Robert Glebocki and Mariusz Jacewicz    
The development of projectile guidance requires consideration of a large number of possible flight scenarios with various system parameters. In this paper, the Monte-Carlo parametric study for a 160 mm artillery rocket equipped with a set of 34 small, so... ver más
Revista: Aerospace    Formato: Electrónico

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