US2012055990A1PendingUtilityA1
Method of Applying Soft-Kill Deployment, a Soft-Kill Deployment System and a Computer Program Product
Est. expiryDec 31, 2028(~2.5 yrs left)· nominal 20-yr term from priority
F42B 12/70F41J 2/02F42B 5/15F41H 11/02
43
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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.
Claims
exact text as granted — not AI-modified1 - 9 . (canceled)
10 . 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.
11 . The method according to claim 10 , wherein an predicted miss distance are based on incoming missile parameters, mother platform parameters and the corresponding decoy launch parameter set.
12 . The method according to claim 10 , wherein the adjoint algorithm includes linearizing a non-linear prediction model.
13 . The method according to claim 10 , wherein the deducing step includes the use of computed uncertainty data corresponding with a predicted zero-effort miss distance.
14 . The method according to claim 10 , further comprising the step of signaling an incoming missile.
15 . The method according to claim 10 , further comprising the step of identifying a signalled incoming missile.
16 . 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.
17 . 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.Cited by (0)
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