FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, namely to aircrafts of vertical take-off and landing – multirotors with increased mobility and compactness. A vertical take-off and landing multi-rotor with impeller thrusters includes independently operating electric engines of carrying impellers, electronic stroke controllers (ESC), accumulator batteries (AB) and an onboard flight computer with a proportional-integral-differentiating regulator (PID-regulator).
EFFECT: compactness and mobility are provided, the safety of an aircraft is increased, and the efficiency of thruster operation is increased.
2 cl, 1 dwg
