FIELD: control systems of flying vehicles, unmanned flying vehicles in particular.
SUBSTANCE: proposed unmanned flying vehicle has fuselage with radioparent fairing, engine plant, control system including homing head located under nose fairing, aerodynamic surfaces and at least one strap-on propellant tank. Strap-on propellant tank is provided with aerodynamic fairing secured on the outside forming space for equipment of additional passive wide-range channel for homing head electrically connected with control system. Aerodynamic fairing possesses radioparent characteristics optimized for operation of additional channel equipment.
EFFECT: increased probability of target lock-on.
1 dwg
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