| 摘要 |
A method of landing an aircraft, according to which engines of aircraft are turned on and then they are decelerated in a predetermined landing area. Deceleration is carried out by a created artificial air flow from a gas dynamic installation, which is basic one, the aircraft is directed on a tangent to the axis of the artificial air flow, speed of which is reduced to zero when the centre of mass of an aircraft enters the space over a given area of landing. At the same time an additional gas dynamic installation is turned on and an additional artificial air flow is created, and the aircraft engines are turned off and the aircraft is fixed when touching the given landing area. |
