Abstract: A retransmitted Ground Positioning System (GPS) using retransmission of a GPS signal in combination with an interferometer for determining the angular deviations of an aircraft relative to a landing site in both vertical and horizontal planes, by using the accumulated phase of the GPS carrier signal. The system includes an aircraft and a landing site, wherein a first unit comprising one of the aircraft and the landing site includes a GPS retransmitter for retransmitting GPS signals to a second unit comprising the other of the aircraft and the landing site, which includes a GPS receiver/computer two spaced apart GPS antennas mounted on a rotating frame, the plane of rotation of which is normal to the landing strip. In a first general configuration, each GPS antenna in the interferometer comprises a GPS receiving antenna and a GPS transmitting antenna, and an amplifier connecting the GPS receiving antenna with the GPS transmitting antenna, and the aircraft includes a GPS receiver/computer.

Abstract: A system for measuring the relative positions of first and second units includes a re-transmitting apparatus at the first unit and a receiver at the second unit capable of making simultaneous real-time comparisons of phase and frequency information contained in first signals received directly from the satellites by the second unit and second signals received from the satellites by the first unit and immediately retransmitted to the second unit in their entirety without processing before retransmission.