In the new technologies for producing electricity from wind gusts, a new class of wind power converter has been proposed. The hybrid autogyro uses the principle of autorotation to generate lift. This paper proposes to take advantage of this rotation to also generate energy. There are systems that use flying wings or airplanes to reach winds that blow in layers of the atmosphere that are inaccessible to traditional wind turbines. Wind gusts are disturbances that significantly affect the behavior of this kind of aircraft. However wind gust is the source of energy and this wind speed increases with the aircraft's altitude. This paper reviews the mathematical model of the hybrid autogyro aircraft and proposes a control algorithm to ensure that the vehicle remains horizontal in forward flight, in this way is possible to maximize the generated energy, this concept is tested in numerical simulations. Symbol Description a 0 , a 1 , b 1 Coning, forward, and side flapping angles. F Force vector [X Y Z] T. g acceleration due to gravity. H Angular momentum vector. I xx , I yy , I zz Inertia matrix components. K p , K i , K d Gain of control terms. L, M, N Torques around x, y and z axes. m Autogyro mass. p N, p E, p D Inertial frame positions (north, east, and down). P, Q, R Body rotation rates about x, y, and z directions. R Rotational matrix, body to inertial frame. T AF Total aerodynamic force. U, V, W Linear velocities in x, y, and z axes. v Velocity vector [U V W] T. X, Y, Z Forces in x, y, and z directions. δ Deflection angle of elevator. τ Torque vector [L M N] T. ν Noise. φ, θ, ψ Euler angles (roll, pitch, yaw). ω Body rotation rate vector [P Q R] T. Ω 3,4 Matrices of rotation rates. (•) A Aerodynamic. (•) a Air relative. (•) d Desired angle. (•) w Air relative velocities. (•) i Inertial frame. (•) e Error. (•) f us Fuselage. (•) ht Horizontal tail. (•) pid Proportional, integral and derivative terms. (•) r Rotor. (•) vt Vertical tail.
