Abstract:
In some example embodiments, there is provided an apparatus comprising an antenna configured to receive a signal from a global navigation satellite system, wherein the antenna includes a first feed and a second feed; a hybrid coupler including a first hybrid input, a second hybrid input, a first hybrid output, a second hybrid output, wherein the first hybrid input is coupled to the first feed, the second hybrid input is coupled to the second feed, and wherein the first hybrid output is shifted in phase by 90 degrees relative to the second hybrid output; a variable phase shifter including a shifter input and a shifter output, wherein the shifter input is coupled to the first hybrid output, wherein variable phase shifter is configured to induce an additional phase shift; and a combiner including a first combiner input, a second combiner input, and a combiner output, wherein the first combiner input is coupled to the shifter output, and the second combiner input is coupled to the second hybrid output, and wherein the combiner output represents a combined right hand circularly polarized signal and left hand circularly polarized signal, wherein the combiner output is provided to detection circuitry. Related systems, methods, and articles of manufacture are also disclosed.
Abstract:
A GPS reference system and corresponding method utilizing a network of reference stations and a master station (Fig. 1). Each reference station (102) receives GPS signals from GPS satellites (106), it observes and computes in response a pseudo-range residual for each GPS satellite. The master station (108) is in communication with the reference stations to receive the computed pseudo-range residuals and comprises a pseudo-range residual synchronizer, an ephemeris and clock correction estimator for each GPS satellite observed by the reference stations and a transmitter. The pseudo-range residual synchronizer computes clock differences between the reference stations so as to synchronize them. Each ephemeris and clock correction estimator computes an ephemeris correction and a clock correction for the corresponding GPS satellite. The transmitter transmits to users the computed ephemeris and clock correction.