Gyroscopic stabilizing device for a projectile control instrument
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United States of America Patent
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-
May 8, 1990
Grant Date -
N/A
app pub date -
Nov 3, 1988
filing date -
Nov 6, 1987
priority date (Note) -
Expired
status (Latency Note)
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Abstract
Disclosed is a device used to bend the end of the trajectory of a rocket in the desired plane without making costly and complicated servo-control mechanisms necessary. A cardan type assembly is formed by a section of the projectile and an internal frame, a gyrostat being mounted in the internal frame. The section carries the control instrument. The device can thus be used to keep the control instrument in a stable roll position throughout the trajectory. It is thus possible to bend the trajectory in a defined direction so as to attack targets from the top with high precision. The device can be adapted to infantry rockets, aeronautical rockets and in general, to short-range projectiles.
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