Manned aircraft control method

The invention discloses a control method of a manned aircraft, and relates to the technical field of aircraft equipment. Thrust is generated through seven micro turbojet engines on the aircraft to keep the aircraft flying; the thrust generated by the seven micro turbojet engines is controlled by adjusting the accelerator; a thrust vectoring nozzle at an output port of the micro turbojet engine E5 is adjusted to assist front and back control of the aircraft; the thrust vectoring nozzles at the output ports of the four micro turbojet engines E1, E2, E3 and E4 are adjusted to control the front-back and left-right hybrid control of the aircraft; the course adjustment of the aircraft is controlled by adjusting thrust vectoring nozzles at output ports of the micro turbojet engines E6 and E7 on the two sides of the aircraft; and the flight attitude of the aircraft is obtained through the gyroscope, so that stable control on the manned aircraft can be realized. 本发明公开了一种载人飞行器的控制方法，涉及飞行器设备技术领域，所述载人飞行器的控制方法包括；通过飞行器上的七个微