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公开(公告)号:US20180356532A1
公开(公告)日:2018-12-13
申请号:US15777035
申请日:2016-11-18
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Sung Hyuck IM , Moon Beom HEO , Eun Sung LEE
CPC classification number: G01S19/42 , B64C39/02 , B64C39/024 , B64C2201/12 , G01S19/03 , H04W64/00
Abstract: An apparatus for determining a precise location including: a plurality of unmanned aerial vehicles each having a first broadband signal module and a global position system GPS receiver attached thereonto and flying in the air; and a terminal provided at a location and determining the location by communication with the first broadband signal modules. In addition, a method for determining a precise location including: respective GPS receivers receiving GPS signals from artificial satellites and detecting locations of each of the plurality of unmanned aerial vehicles, transmiting locations of the unmanned aerial vehicles and distances between the unmanned aerial vehicles and the terminal and determining a location of the terminal using information received from the first broadband signal modules.
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公开(公告)号:US20180143325A1
公开(公告)日:2018-05-24
申请号:US15819926
申请日:2017-11-21
Applicant: KOREA AEROSPACE RESEARCH INSTITUTE
Inventor: Jae Ik PARK , Eun Sung LEE , Moon Beom HEO , Gi Wook NAM
Abstract: A Global Positioning System (GPS) receiver, a control method of the GPS receiver, and a GPS system are provided, which are capable of reducing an initial position check time using an SBAS signal transmitted from a SBAS satellite. The control method of a GPS receiver includes receiving an SBAS signal from a SBAS satellite and calculating a satellite clock and a satellite position of the GPS receiver using the received SBAS signal. The SBAS signal may contain a difference value between the ephemeris data and the almanac data of the GPS satellite. The difference value between the ephemeris data and the almanac data may include a satellite clock difference value and a satellite position difference value for the GPS satellite. Accordingly, it is possible to acquire the current position and time information more quickly and accurately, by shortening the initial position check time using the difference value between the ephemeris data and the almanac data included in the SBAS signal.
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公开(公告)号:US20170184723A1
公开(公告)日:2017-06-29
申请号:US15342431
申请日:2016-11-03
Applicant: Korea Aerospace Research Institute
Inventor: Young Sun YUN , Eun Sung LEE , Moon Beom HEO , Gi Wook NAM
Abstract: Disclosed is a system for determining a protection level. The system includes a receiver configured to receive an error augmentation for a satellite orbit and clock error, an error augmentation for an ionospheric error, an error augmentation for noise and multi-path between a receiver and a satellite, and an error augmentation for a tropospheric error, a first calculator configured to calculate a first adjustment coefficient to be applied to the error augmentation for the satellite orbit and clock error and the error augmentation for the ionospheric error, and a second calculator configured to calculate a protection level by applying the first adjustment coefficient.
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