Method and apparatus for determining the position and orientation of a missile
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United States of America Patent
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Oct 25, 2011
Grant Date -
Sep 4, 2008
app pub date -
Oct 11, 2006
filing date -
Oct 20, 2005
priority date (Note) -
Expired
status (Latency Note)
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Abstract
A system for determining the position and orientation of a flying object such as a missile includes a ground segment having at least one pseudolite station located on the earth's surface which transmits into space a navigation signal that uniquely identifies the pseudolite station, and a user segment having at least one sensor which is situated in the missile and is designed to receive the navigation signal from the at least one pseudolite station and to determine its absolute position and orientation in space on the basis of the received navigation signal.
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