Method of correcting the trajectory of a spin-stabilised projectile and projectile implementing one such method
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United States of America Patent
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Issued Date -
Aug 11, 2005
app pub date -
Dec 7, 2004
filing date -
Nov 8, 2002
priority date (Note) -
Abandoned
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Abstract
The invention relates to a process to correct the trajectory of a spin-stabilised projectile, process in which at least one correction is made to the axial position of the projectile's centre of aerodynamic thrust, such process wherein the correction of the axial position of the centre of thrust is obtained by modifying at least once the length of the projectile in flight, such modification being triggered by control means.
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