Maximum-likelihood rocket identifier
AssigneeLockheed Martin Corporation
InventorJeffrey B. Boka
Life of this patent
Estimating the term…
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AssigneeLockheed Martin Corporation
InventorJeffrey B. Boka
Estimating the term…
A sensor suite determines location and velocity information relating to a missile threat, which is converted to missile or rocket state estimates. The state estimates are transformed into time-invariant dynamic parameters, unique for each missile type. Estimated rocket dynamic parameters are computed for each target type being considered, and compared with a reference set of rocket parameters representing different target types. The estimated rocket parameters are compared with the reference parameters in a maximum-likelihood sense, and combined using fuzzy logic to identify the rocket type and the likelihood. The identified rocket type and likelihood is used to aid in determining the future location of the missile so countermeasure can be applied.
A method for estimating at least one of the type and future location of a missile based on information relating to its sensed present position and velocity, said method comprising the steps of:
A method for estimating the future location of a missile based on information relating to its sensed present position and velocity, said method comprising the steps of:
Dependencies are inferred from the claim text.