FIELD: rocket equipment.
SUBSTANCE: invention relates to the missiles launchers. Using the associated with salvo firing system guides package gyroscopic device, measuring the package angular oscillations after the firing. Issuing the command for the subsequent firing takes place with the package longitudinal axis entering into the specified area around the aiming line or alignment with it. Command is issued taking into account the delay between the command for the firing and the firing.
EFFECT: reduction of multiple rocket launcher system fired missiles spreading.
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Authors
Dates
2018-12-03—Published
2017-10-16—Filed