FIELD: transport.
SUBSTANCE: invention relates to control over the flight path of bodies flying at high speeds including orbital velocities. In compliance with proposed method, this system can be used as a backup (standby) path correction system for missiles with failed guidance system. Besides, it can be used at minor bodies whereat installation of standard self-guidance system causes problems. Proposed method comprises application of silicon strips 5, 6, 7, 8 on body side surface alloyed to different degree that provides for different resonance frequency of laser absorption. Laser radiation 3 getting on strip with resonance frequency of radiation absorption causes its evaporation and occurrence of appropriate correcting reactive force. By varying the radiation frequency 3, to get correction pulses in required directions.
EFFECT: possibility to control flight path in two directions across the vector of its current velocity.
1 dwg
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Authors
Dates
2014-09-20—Published
2012-12-04—Filed