Abstract:
The present invention relates to a positioning system using a GNSS and a control method thereof. In a method for a terminal supporting a GNSS to perform location determination technology related with one embodiment of the present invention, the method includes the steps of: receiving first information from a first receiver; receiving second information from an international GNSS service (IGS); and outputting third information related with a position of the first receiver using the first information and the second information. The first receiver is one, and is a receiver which is not included in an IGS network related with the IGS. The first information may be information related with a radio wave which the first receiver receives from at least one satellite included in the GNSS. [Reference numerals] (510) Input; (530) Output; (540) IGS final predicted position table (Final ephemeris); (AA) Rinex file; (BB) Daily update; (CC) Prefilter; (DD) Error models; (EE) Stochasticmodels; (FF) EKF or recursive LS; (GG) Daily or yearly update; (HH) Ocean loading data; (II) DCB data; (JJ) PCO and PCV data; (KK) MET data; (LL) ECEF coordinate; (MM) Clock bias
Abstract:
본 발명은 글로벌 위성 항법 시스템을 이용한 전리층 내의 총전자량과 DCB 측정시스템, 측정방법 및 그 기록매체에 대한 것이다. 보다 상세하게는, 글로벌 위성 항법 시스템을 이용한 전리층 내의 총전자량과 DCB 측정시스템에 있어서, 위성으로부터 위성신호를 수신받는 GNSS 수신기; 및 GNSS 수신기에서 수신받은 위성신호를 전송받고, 전송받은 위성신호를 기반으로 GNSS 수신기의 상공에 위치한 전리층 내의 총전자량과 DCB 모두를 실시간으로 측정하는 측정수단;을 포함하는 것을 특징으로 하는 글로벌 위성 항법 시스템을 이용한 전리층 내의 총전자량과 DCB 측정시스템에 관한 것이다.
Abstract:
The present invention relates to an apparatus for monitoring system time differences of a GNSS and a control method thereof. In a method in which a multi global navigation satellite system (multi-GNSS) using a plurality of satellite position measuring systems related with one embodiment of the present invention monitors time differences of each of the plurality of satellite positioning systems. The method of the present invention may include: a first step of setting a first station in the multi-GNSS as a reference station; a second step in which the reference station transmits first time information to a second station most adjacent to the reference station; a third step of judging whether the second station is a final station or not; and a fourth step of calculating time difference of each of the plurality of satellite position measuring systems using the first time information if the second station is the final station, and setting the second station as the reference station newly if the second station is not the final station. [Reference numerals] (AA) START; (BB) END; (S410) Step of setting first station on link as reference station; (S420) Step of transmitting time information to most adjacent unused station from reference station; (S430) Step of setting destination station as new reference station; (S440) Whether arrives at final station; (S450) Step of summing all time transmission results to acquire time difference solution
Abstract:
The present invention relates to a system and a method for measuring total electron content in an ionosphere and differential code bias (DCB) using a global navigation satellite system (GNSS) and a recording medium thereof. More particularly, the system for measuring total electron content in the ionosphere and DCB using the GNSS includes: a GNSS receiver receiving a satellite signal from a satellite; and a measuring unit which receives the satellite signal received in the GNSS receiver, and measures total electron content in the ionosphere located in the upper air of the GNSS receiver and the DCB in real-time on the basis of the received satellite signal. [Reference numerals] (10) GNSS receiver;(21) TEC measurement module;(22) DCB measurement module
Abstract:
The present invention relates to a system and a method for measuring the amount of vapor in atmosphere layer using a global differential GPS and a recording medium for the same. More specifically, the system for measuring the amount of vapor in atmosphere layer using the global differential GPS comprises a plurality of client GNSS receivers, a server, and a server GNSS receiver. The plurality of client GNSS receivers receives first satellite signals from each satellite. The server receives the satellite signals from each client GNSS receiver. The server GNSS receiver separately formed in the server from the client GNSS receiver receives second satellite signals from the satellite and transmits the second satellite signals to the server. The server calculates a first signal delay value from each first satellite signal from the client GNSS receivers. The server measures the amount of vapor in the atmosphere layer wherein the client GNSS receivers are positioned based on the first signal delay value. The server calculates a second signal delay value from the second transmitted satellite signals and measures the amount of vapor in the atmosphere layer based on the second signal delay value. [Reference numerals] (10) Server;(20) Server GNSS receiver
Abstract:
The present invention relates to a positioning system using a global navigation satellite system (GNSS), a positioning method thereof and a recording medium thereof. More specifically, in a positioning system using a GNSS, the present invention relates to a positioning system including: a number of client GNSS receivers which receive a first satellite signal from a satellite respectively; a server receiving the satellite signal received by each GNSS receiver; and a server GNSS receiver which is comprised in the server separately from the client GNSS receiver and receives a second satellite signal from the satellite and then transmits the received second satellite signal to the server. The server measures precise position information of centimeter level as to sever-client distance of several hundreds km level by removing ephemeris error of the satellite and correcting troposphere delay through Stochastic method with a model. [Reference numerals] (10) Server;(20) Server GNSS receiver