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A review of dual-spin projectile stability
Institution:1. Centre for Defence Engineering, Cranfield University, Defence Academy of the United Kingdom, Shrivenham, SN6 8LA United Kingdom;2. BAE Systems, United Kingdom
Abstract:This paper gives a succinct review of dual-spinprojectile stability and some technologies relating to them. It describes how the traditional stability factors from linear projectile theory are modified to better describe a controlled dual-spin projectile. Finally, it reviews works which have investigated how different aspects of a controlled dual-spin design can affect flight stability, primarily airframe structure and canard properties. A conclusion is given, highlighting important guidelines from the enclosed discussions.
Keywords:Guided projectiles  Dual-spin  Gyroscopic  Dynamic  Stability  Canards
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