Method and guidance system for guiding a missile
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United States of America Patent
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Jan 6, 2004
Grant Date -
N/A
app pub date -
Apr 24, 2002
filing date -
Aug 18, 1999
priority date (Note) -
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Abstract
The present invention relates to a method and an arrangement for guiding a missile. In accordance with the prior art, the angle position of a target (9) when the missile (3) is expected to reach the target is predicted on the basis of the angular velocity determined in a preceding time period. In order to improve the strike accuracy, the operator, in a second subsequent time period, tracks the actual position of the missile in relation to the predicted angle position of the target. If a deviation is observed, a correction command is transmitted to the missile in order to correct the missile trajectory. For this purpose, a communications link is provided to transmit the correction command given by the operator.
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