发明名称 SATELLITE ORBITAL DETERMINATION (OD) USING DOPPLER AND KEPLER ORBITAL ELEMENTS
摘要 <p>Technology to determine a satellite's orbit is disclosed. In an example, an orbital determination (OD) device for a satellite operable to determine a satellite's orbit can include computer circuitry configured to: Receive a single global positioning system-generated (GPS-generated) signal from a GPS satellite; decode an ephemeris of the GPS satellite from the GPS-generated signal; determine a Doppler shift and a Doppler trend of the GPS-generated signal; and generate a Doppler-GPS OD using the ephemeris of the GPS satellite and the Doppler shift and the Doppler trend of the GPS-generated signal fit to Kepler orbital elements of an orbit model.</p>
申请公布号 WO2014194128(A3) 申请公布日期 2015.04.09
申请号 WO2014US40077 申请日期 2014.05.29
申请人 RAYTHEON COMPANY 发明人 ROBINSON, IAN S.
分类号 B64G1/24;B64G1/36;G01S19/38;G01S19/39 主分类号 B64G1/24
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