The invention discloses a flying
robot with variable sweep angle launch tandem wings and aims to solve the problem that neither two front folding wings nor two rear folding wings of an existing launch flying
robot can be unfolded respectively, so that moving
attitude control of the flying
robot is limited. The flying robot comprises a
folding propeller, a
fuselage, a left rear wing, a right rear wing, a left front wing, a right front wing, two vertical tails, two vertical
tail pin shafts and four rotary hinges, wherein the
folding propeller is installed on the head of the
fuselage, the left front wing and the right front wing are symmetrically arranged on the two sides of the front end of the
fuselage, the left rear wing and the right rear wing are symmetrically arranged on the two sides of the rear end of the fuselage, the left front wing, the right front wing, the left rear wing and the right rear wing are hinged to the corresponding rotary hinges respectively, each rotary hinge is connected with a corresponding helm gear in the fuselage, and the two vertical tails are symmetrically arranged on the two sides of the
tail end of the fuselage and installed on the upper surface of the
tail portion of the fuselage through torsional springs. The flying robot is used for
attitude control.