A Global Navigation Satellite System (GNSS) receiver for processing satellite signals with integer cross ambiguity resolution. The receiver includes an antenna assembly receiving signals from a set of GNSS satellites. The receiver includes a transceiver establishing a communication link with a spaced-apart GNSS receiver and receiving data from the spaced-apart GNSS receiver to make up a base station and rover pair performing DD techniques. The receiver includes a processor and a cross ambiguity fixing module provided by the processor executing code to generate an error correction. The receiver includes an estimator provided by the processor executing code to provide a geographical position solution by DD processing the data from the space-apart GNSS receiver and the signals from the set of GNSS satellites along with the error correction, which may provide a search space with more DD ambiguities or may address quarter or half cycle bias between receiver types.

A Global Navigation Satellite System (GNSS) receiver for processing satellite signals with integer cross ambiguity resolution. The receiver includes an antenna assembly receiving signals from a set of GNSS satellites. The receiver includes a transceiver establishing a communication link with a spaced-apart GNSS receiver and receiving data from the spaced-apart GNSS receiver to make up a base station and rover pair performing DD techniques. The receiver includes a processor and a cross ambiguity fixing module provided by the processor executing code to generate an error correction. The receiver includes an estimator provided by the processor executing code to provide a geographical position solution by DD processing the data from the space-apart GNSS receiver and the signals from the set of GNSS satellites along with the error correction, which may provide a search space with more DD ambiguities or may address quarter or half cycle bias between receiver types.

A navigation processing system includes at least one processor configured to execute operational instructions that cause the at least one processor to perform operations that include generating navigation data. A data stream is generated based on the navigation data and a data channel spreading sequence. A pilot stream is generated based on a pilot channel spreading sequence. A navigation signal is generated based on applying a bandwidth-efficient modulation scheme to the data stream and the pilot stream. The navigation is signal is broadcast via a navigation signal transmitter for receipt by at least one client device.

A navigation processing system includes at least one processor configured to execute operational instructions that cause the at least one processor to perform operations that include generating navigation data. A data stream is generated based on the navigation data and a data channel spreading sequence. A pilot stream is generated based on a pilot channel spreading sequence. A navigation signal is generated based on applying a bandwidth-efficient modulation scheme to the data stream and the pilot stream. The navigation is signal is broadcast via a navigation signal transmitter for receipt by at least one client device.

A PVT calculation device includes a memory; and one or more processors in communication with the memory configured to perform operations including: receiving observations and ephemerides from satellites to obtain PVT data of the satellites and predicted PVT results of the receiver; setting up observation functions respectively corresponding to the satellites; calculating by a least square solution first estimated PVT results of the receiver based on the observation functions; iteratively eliminating by a Random-Sampling Iterative Kalman Filter (RSIKF) algorithm fault observation functions from the observation functions in an inner cluster until no fault observation functions detected in the inner cluster; calculating by the RSIKF algorithm a second estimated PVT results of the receiver using the observation functions in the inner cluster; and outputting final estimated PVT results of the receiver. The PVT calculation device may calculate the PVT results of the receiver with improved accuracy and stability.

A time-differenced carrier phase (TDCP) measurement value-based navigation system according to one embodiment of the present invention comprises: a satellite navigation system information reception unit for acquiring satellite navigation system information including a carrier phase measurement value; an initial position determination unit for determining an initial position of a target on the basis of the satellite navigation system information; a TDCP acquisition unit for acquiring a TDCP measurement value; a relative position determination unit for determining a relative position of the target on the basis of the TDCP measurement value; and an absolute position determination unit for determining an absolute position of the target by accumulating relative positions according to time of the initial position of the target. According to an embodiment, unlike a conventional navigation system, a position of the target is determined on the basis of a TDCP measurement value, and thus an accurate position of the target can be determined even without calculating integer ambiguity. Therefore, time and expenses required for determining integer ambiguity can be reduced, and precise position of a cm-level error can be measured by using a low-cost satellite navigation system information receiver.

A time-differenced carrier phase (TDCP) measurement value-based navigation system according to one embodiment of the present invention comprises: a satellite navigation system information reception unit for acquiring satellite navigation system information including a carrier phase measurement value; an initial position determination unit for determining an initial position of a target on the basis of the satellite navigation system information; a TDCP acquisition unit for acquiring a TDCP measurement value; a relative position determination unit for determining a relative position of the target on the basis of the TDCP measurement value; and an absolute position determination unit for determining an absolute position of the target by accumulating relative positions according to time of the initial position of the target. According to an embodiment, unlike a conventional navigation system, a position of the target is determined on the basis of a TDCP measurement value, and thus an accurate position of the target can be determined even without calculating integer ambiguity. Therefore, time and expenses required for determining integer ambiguity can be reduced, and precise position of a cm-level error can be measured by using a low-cost satellite navigation system information receiver.

A system and method for detecting spoofing of a Global Navigation Satellite System (GNSS) system using a plurality of antennas. Signals received by at least two of the plurality of antennas are authentication by use of one or more of a carrier phase authentication procedure, a signal power authentication procedure, and/or a channel distortion authentication procedure.

A system and method for detecting spoofing of a Global Navigation Satellite System (GNSS) system using a plurality of antennas. Signals received by at least two of the plurality of antennas are authentication by use of one or more of a carrier phase authentication procedure, a signal power authentication procedure, and/or a channel distortion authentication procedure.

A wireless device determines a biased wireless device position and a receiver clock error for a plurality of satellites, the biased wireless device position and the receiver clock error being associated with a biased ambiguity. The wireless device calculates, upon determining the biased wireless device position and the receiver clock error, the biased ambiguity for each of the plurality of satellites. The wireless device applies the biased ambiguity to a carrier phase measurement for each of the plurality of satellites, the carrier phase measurement being associated with the receiver clock error and an absolute location of the wireless device. The wireless device determines, upon applying the biased ambiguity to the carrier phase measurement for each of the plurality of satellites, the absolute location of the wireless device based on the biased ambiguity for all of the plurality of satellites.