FIELD: rocket equipment.
SUBSTANCE: group of inventions relates to the field of guided missile weapon application and can be used in multichannel complexes having means of detecting, tracking targets and direction finding of missiles. Method involves detecting, capturing and tracking several targets, assigning each target to each missile by specifying a channel interval. After each missile is tied to its target and a command is received to launch the missile, the on-board missile equipment is ready to record repeating code parcels. In each premise, a set of parameters of the corresponding channel interval target, which are used in the control system when transmitting commands to the missile and receiving response signals from it, as well as the target type are generated. Recording is performed until its confirmation from on-board equipment of missile. Then, the recorded set of parameters is read out and compared with the transmitted set. In case of their match, write-reading of parameters is terminated and rocket is launched with further controlled flight. In case of discrepancy of set of parameters recorded in on-board equipment, transmitted write-reading procedure is repeated for preset time. If the set of parameters does not match, the missile is launched without flight control with subsequent self-liquidation.
EFFECT: shorter time for checking readiness of missile before launch.
2 cl, 1 dwg
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Authors
Dates
2019-05-23—Published
2018-05-29—Filed