| 摘要 |
An unmanned aircraft with an electric power unit has a fuselage with a tail, a direct non-mechanized wing with aerodynamic profile of low relative thickness and a surveillance camera, which is located underneath the fuselage. In the unmanned aircraft a landing parachute is used, three-point spring chassis with a tail support with developed main supports, and its wing is made with negative sweep and equipped with mechanization. |
