FIELD: aviation; instrumentation.
SUBSTANCE: rocket missile (1) is equipped with homing head (2) with a homing system on the basis of a gimballess navigation system, characterised by the target capture stage, during which it attempts to detect target (C), and which is characterised by direction (3) of vision, wherein said direction (3) of vision is fixed relative to rocket missile (1) and is directed along longitudinal axis (4) of the latter, and said missile (1) additionally contains control means (8) for automatic control of said missile (1) so that its longitudinal axis (4) in flight during the stage of capture by homing head (2) makes a circle whose radius is increased in time until target (C) is detected.
EFFECT: higher efficiency of homing systems.
5 cl, 2 dwg
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