Aircraft support leg, aircraft and control method

A control method of an aircraft support leg, being characterized in, the aircraft support leg rotatably disposed on or in a main body of an aircraft, the method comprising:

• rotating the aircraft support leg from a first position, at which an angle is between the aircraft support leg and the main body of the aircraft, to a second position, at which the aircraft support leg is stowed and substantially abuts against a housing of the main body of the aircraft;
• or
• rotating the aircraft support leg from the first position, at which the angle is between the aircraft support leg and the main body of the aircraft, to the second position, at which the aircraft support leg is at least partially arranged in the housing of the main body of the aircraft.

A control method of an aircraft support leg, the aircraft support leg rotatably disposed on or in a main body of an aircraft, the method comprising:

• extending the aircraft support leg from a second position, at which the aircraft support leg substantially abuts against a housing of the main body of the aircraft, to a first position, at which an angle is between the aircraft support leg and the main body of the aircraft;
• or extending the aircraft support leg from the second position, at which the aircraft support leg is in the housing of the main body of the aircraft, to the first position, at which the angle is between the aircraft support leg and the main body of the aircraft.