Systems and methods are disclosed for implanting a dual-kite aerial vehicle including a first kite apparatus, a second kite apparatus, and a tether extending between the first and second kite apparatuses. In particular, the disclosed systems include a first kite apparatus including a first flight controller that maintains flight at a first altitude. The disclosed system further includes a second kite apparatus including a second flight controller that maintains flight at a second altitude. The flight controllers can cooperatively maintain a gradient air movement between the first and second altitudes by extending or retracting the tether to modify a difference in the air movements between the first and second kite apparatuses. The systems described herein additionally include components for generating electrical energy from the gradient air movement to extend a flight time of the dual-kite aerial vehicle.

Systems and methods are disclosed for implanting a dual-kite aerial vehicle including a first kite apparatus, a second kite apparatus, and a tether extending between the first and second kite apparatuses. In particular, the disclosed systems include a first kite apparatus including a first flight controller that maintains flight at a first altitude. The disclosed system further includes a second kite apparatus including a second flight controller that maintains flight at a second altitude. The flight controllers can cooperatively maintain a gradient air movement between the first and second altitudes by extending or retracting the tether to modify a difference in the air movements between the first and second kite apparatuses. The systems described herein additionally include components for generating electrical energy from the gradient air movement to extend a flight time of the dual-kite aerial vehicle.

The present invention provides a method of manufacturing a kite including: forming a body wherein the body includes a wing, a material of the body being made of a blister material; and forming a supporting member by blistering the wing, whereby the supporting member is formed directly from the wing, wherein the supporting member is integrally formed with the wing and maintains a shape of the body.

The present invention provides a method of manufacturing a kite including: forming a body wherein the body includes a wing, a material of the body being made of a blister material; and forming a supporting member by blistering the wing, whereby the supporting member is formed directly from the wing, wherein the supporting member is integrally formed with the wing and maintains a shape of the body.

A morphing aerodynamic structure includes a body with an outer covering, a bridle attached to the body, and a light-response polymer disposed on at least one of the outer covering and the bridle. The light-responsive polymer is configured to change shape when illuminated with a laser such that at least one of an angle of attack, roll, pitch and yaw of the morphing aerodynamic structure is at least partially controlled without the use of a mechanical or pneumatic control unit.

A morphing aerodynamic structure includes a body with an outer covering, a bridle attached to the body, and a light-response polymer disposed on at least one of the outer covering and the bridle. The light-responsive polymer is configured to change shape when illuminated with a laser such that at least one of an angle of attack, roll, pitch and yaw of the morphing aerodynamic structure is at least partially controlled without the use of a mechanical or pneumatic control unit.

A kite control system for controlling a kite which includes a plurality of rotators, a plurality of guiding elements locatable between each of the plurality of rotators and the kite, a plurality of adjustable deflectors, a plurality of deflector guides configured to adjust the operational length of the kite connecting line upon adjustment of the deflector, at least one invert correlator for, when in use, inversely correlate the adjustment of the operative length of the respective kite connecting lines, wherein the plurality of kite connecting lines includes the connection of at least one of the kite connecting lines at the kite biased towards the leading end region of the kite, and the connection of at least another kite connecting line biased towards the trailing end region of the kite.

A kite control system for controlling a kite which includes a plurality of rotators, a plurality of guiding elements locatable between each of the plurality of rotators and the kite, a plurality of adjustable deflectors, a plurality of deflector guides configured to adjust the operational length of the kite connecting line upon adjustment of the deflector, at least one invert correlator for, when in use, inversely correlate the adjustment of the operative length of the respective kite connecting lines, wherein the plurality of kite connecting lines includes the connection of at least one of the kite connecting lines at the kite biased towards the leading end region of the kite, and the connection of at least another kite connecting line biased towards the trailing end region of the kite.

A kite control bar having a tensioning member anchored to the bar end float and secured to the trim line. The tensioning member is capable of expanding and contracting. The tensioning member has a default state which is either an expanded state or a contracted state. When an adjusting force is exerted upon the trim line, the tensioning member is drawn into another of the expanded state or the contracted state. When the adjusting force is released, the tensioning member tends to return to the default state. This biases the trim line to force excess trim line out of the bar end float.

A kite leading edge has a tubular structure having a first curve in a span-wise direction and a second curve a chord-wise direction. The tubular structure is formed by a plurality of panels joined together at seams including at least a first longitudinal seam running in the span-wise direction of the tubular structure. At least a portion of the first longitudinal seam defines a first partial helical path about the circumference of the tubular structure.