FIELD: weapons and ammunition.
SUBSTANCE: proposed method is used for testing the rocket at test station or at technical position for real time control over standard rocket or its versions as well as components, particular, self-guidance head and inertial control system, without rocket disassembly. Proposed method allows testing the rocket operation at prelaunch preparation and lunch, independent flight and expanded control over rocket components, particularly, self-guidance head and inertial control system, and self-control of tester. It allows the control over data exchange between rocket and carrier hardware at prelaunch preparation and lunch, independent flight and expanded control over rocket components, and simulation of independent flight and background-target situation. Method cam be used for testing the rocket incorporating digital data exchange interfaces.
EFFECT: higher reliability and validity.
5 cl, 2 dwg
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Authors
Dates
2013-11-27—Published
2012-04-28—Filed