Abstract: The object of the present invention is to provide a device that allows the intermittent operation of the cooling fan, with a mechanism controlled by the stator temperature, to reduce whipping losses and improve the operating efficiency of three-phase induction motors for industrial use, such as those that operate pumps, compressors, conveyors, fans, welding machines and die cutters, among others.

Abstract: Systems and methods for determining navigation information for an aircraft are provided. In one embodiment, a method can include accessing a satellite-based positioning signal received at a receiver on an aircraft. The satellite-based positioning signal can be indicative of a distance between a satellite and the receiver. The method can include identifying from the satellite-based positioning signal a first vector associated with a distance between the satellite and the receiver and identifying a second vector from the satellite-based positioning signal associated with a distance between a reference point and the satellite. The method can include generating a kinematic model for determining a geometric position of the aircraft based at least in part on a robotic arm using the first vector and the second vector and determining navigation information for the aircraft based at least in part on the kinematic model.

Abstract: Systems and methods for determining navigation information for an aircraft are provided. In one embodiment, a method can include accessing a satellite-based positioning signal received at a receiver on an aircraft. The satellite-based positioning signal can be indicative of a distance between a satellite and the receiver. The method can include identifying from the satellite-based positioning signal a first vector associated with a distance between the satellite and the receiver and identifying a second vector from the satellite-based positioning signal associated with a distance between a reference point and the satellite. The method can include generating a kinematic model for determining a geometric position of the aircraft based at least in part on a robotic arm using the first vector and the second vector and determining navigation information for the aircraft based at least in part on the kinematic model.