FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to aircraft systems for collecting information. The multifunctional aerodynamic distributed system comprises a plurality of vertical take-off and landing unmanned aircraft, each of which comprises an air propeller of the adjustable step arranged in the head part of the fuselage and an automatic wheel, and a tail chassis, ensuring the vertical position of the fuselage during take-off and landing. In flight the chassis is folded to form a conical tail fairing. There is no tail fin. Control of the aircraft is carried out by changing the cyclic step of the propeller and the ailerons. The communication system is constructed using optical communication between adjacent parts of the system within the limits of direct visibility. It is also used as a system for navigating and positioning individual elements using triangulation at reference points.
EFFECT: ensured is increase in the range of action of the system, the resistance to interference and survivability under conditions of active counteraction.
1 cl, 3 dwg
