The invention relates to a one-point double-shaft multi-propeller aircraft which comprises a fixed bracket, a nacelle, a power shaft, a power rotor, a power motor, an attitude rotor and an attitude motor, wherein the fixed bracket is a transverse and longitudinal crossed bracket which is horizontally arranged, the nacelle is coaxially and fixedly installed on the lower end of the fixed bracket, the power shaft is coaxially installed on the upper end of the fixed bracket, the power rotor which is parallel to the fixed bracket is installed on the power shaft, the power rotor is driven to rotate by the power motor which is installed on the lower part of the power rotor, a coaxial double-propeller structure is adopted, and double propellers are overlapped and vertically arranged. The one-point double-shaft multi-propeller aircraft has the advantages of simple structure, safety, reliability, space saving, convenience in movement and field operation and large air bearing capacity, the posture is controlled by an upper propeller, power is supplied by a plurality of lower propellers, and the work requirements of aerial photos, communication and the like can be fully satisfied.