Abstract: A system may include a tether coupled to a ground station. The system may also include an aerial vehicle coupled to the tether and configured to fly in a given path relative to the ground station based on a length of the tether. The system may also include one or more load cells coupled to the tether and configured to provide information indicative of a tether force between the tether and the aerial vehicle. The one or more load cells may be arranged in a given arrangement indicative of a direction of the tether force. The system may also include a controller configured to determine an angle between a direction of wind incident on the aerial vehicle and a plane defined by a longitudinal axis and a lateral axis of the aerial vehicle based on the tether force.

Abstract: A system may include a tether coupled to a ground station. The system may also include an aerial vehicle coupled to the tether and configured to fly in a given path relative to the ground station based on a length of the tether. The system may also include one or more load cells coupled to the tether and configured to provide information indicative of a tether force between the tether and the aerial vehicle. The one or more load cells may be arranged in a given arrangement indicative of a direction of the tether force. The system may also include a controller configured to determine an angle between a direction of wind incident on the aerial vehicle and a plane defined by a longitudinal axis and a lateral axis of the aerial vehicle based on the tether force.

Abstract: A system may include a tether coupled to a ground station. The system may also include an aerial vehicle coupled to the tether and configured to fly in a given path relative to the ground station based on a length of the tether. The system may also include one or more load cells coupled to the tether and configured to provide information indicative of a tether force between the tether and the aerial vehicle. The one or more load cells may be arranged in a given arrangement indicative of a direction of the tether force. The system may also include a controller configured to determine an angle between a direction of wind incident on the aerial vehicle and a plane defined by a longitudinal axis and a lateral axis of the aerial vehicle based on the tether force.

Abstract: Wind energy systems, such as an Airborne Wind Turbine (“AWT”), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to electrical energy. The aerial vehicle may be tethered to a ground station with a tether that terminates at a tether termination mount system. In one aspect, the tether termination mount system may include a tether termination unit configured in one or more gimbals that allow for the tether termination unit to rotate about one or more axes while tracking the aerial vehicle in flight. In a further aspect, the tether termination mount system may include an imaging device configured for imaging the aerial vehicle during flight in order to enhance tracking accuracy over that which is performed by angular motion of the tether termination unit.

Abstract: Wind energy systems, such as an Airborne Wind Turbine (“AWT”), may be used to facilitate conversion of kinetic energy to electrical energy. An AWT may include an aerial vehicle that flies in a path to convert kinetic wind energy to electrical energy. The aerial vehicle may be tethered to a ground station with a tether that terminates at a tether termination mount system. In one aspect, the tether termination mount system may include a tether termination unit configured in one or more gimbals that allow for the tether termination unit to rotate about one or more axes while tracking the aerial vehicle in flight. In a further aspect, the tether termination mount system may include an imaging device configured for imaging the aerial vehicle during flight in order to enhance tracking accuracy over that which is performed by angular motion of the tether termination unit.