Method of Applying Soft-Kill Deployment, a Soft-Kill Deployment System and a Computer Program Product
AssigneeNederlandse Organisatie voor toegepast-natuurwetenschappelijk onderzoek TNO
InventorsMartin Weiss, Franciscus Aloysius Maria Dam
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Abstract
The invention relates to a method of applying soft-kill deployment to mislead an incoming missile directed to a mother platform. The method comprises the step of predicting a number of miss distances associated with corresponding particular decoy launch parameter sets. Further, the method comprises the step of selecting a decoy parameter set having an optimal predicted miss distance. The method also comprises the step of transmitting the selected decoy parameter set to a launch unit for launching the decoy. Here, the predicting step includes the use of an adjoint algorithm.
Claims9
1-9. (canceled)
A method of applying soft-kill deployment to mislead an incoming missile directed to a mother platform, the method comprising the steps of:
- predicting a number of miss distances associated with corresponding particular decoy launch parameter sets,
- selecting a decoy parameter set having an optimal predicted miss distance;
- and
- transmitting the selected decoy parameter set to a launch unit for launching the decoy;
- wherein the predicting step includes the use of an adjoint algorithm, wherein the method further comprises the step of computing uncertainty data associated with a predicted miss distance, and wherein, in the step of selecting a decoy parameter set, the computed uncertainty data is taken into account,
- further comprising a step of validating the effect of the launched decoy, the validation step comprising the substeps of:
- predicting a zero-effort miss distance, under platform lock on condition and/or decoy lock on condition;
- measuring incoming missile data;
- comparing the measured data with the predicted zero-effort miss distance or distances;
- deducing, from the comparison results, on which entity the incoming missile is locked.
A soft-kill deployment system, comprising:
- a launch unit for launching a decoy to mislead an incoming missile directed to a mother platform, and
- a computer system provided with a processor that is arranged for performing the steps of:
- predicting a number of miss distances associated with corresponding particular decoy launch parameter sets,
- selecting a decoy parameter set having an optimal predicted miss distance;
- and
- transmitting the selected decoy parameter set to the launch unit for launching the decoy;
- wherein the predicting step includes the use of an adjoint algorithm, and wherein the processor is further arranged for performing the step of computing uncertainty data associated with a predicted miss distance, and wherein, in the step of selecting a decoy parameter set, the computed uncertainty data is taken into account,
- wherein the processor is further arranged for performing the step of:
- validating the effect of the launched decoy, the validation step comprising the substeps of:
- predicting a zero-effort miss distance, under platform lock on condition and/or decoy lock on condition;
- measuring incoming missile data;
- comparing the measured data with the predicted zero-effort miss distance or distances;
- deducing, from the comparison results, on which entity the incoming missile is locked.
A computer program product for applying soft-kill deployment to mislead an incoming missile directed to a mother platform, the computer program product comprising computer readable code for causing a processor to perform the steps of:
- predicting a number of miss distances associated with corresponding particular decoy launch parameter sets,
- selecting a decoy parameter set having an optimal predicted miss distance;
- and
- transmitting the selected decoy parameter set to a launch unit for launching the decoy;
- wherein the predicting step includes the use of an adjoint algorithm, wherein the computer program product further comprises computer readable code for causing a processor to perform the step of computing uncertainty data associated with a predicted miss distance, and wherein, in the step of selecting a decoy parameter set, the computed uncertainty data is taken into account,
- and wherein the computer program product comprises computer readable code for causing a processor to perform the steps of:
- validating the effect of the launched decoy, the validation step comprising the substeps of:
- predicting a zero-effort miss distance, under platform lock on condition and/or decoy lock on condition;
- measuring incoming missile data;
- comparing the measured data with the predicted zero-effort miss distance or distances;
- deducing, from the comparison results, on which entity the incoming missile is locked.
Dependencies are inferred from the claim text.