Invention Grant
US09453903B2 Satellite orbital determination (OD) using Doppler and Kepler orbital elements
有权
卫星轨道确定(OD)使用多普勒和开普勒轨道元素
- Patent Title: Satellite orbital determination (OD) using Doppler and Kepler orbital elements
- Patent Title (中): 卫星轨道确定(OD)使用多普勒和开普勒轨道元素
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Application No.: US13904953Application Date: 2013-05-29
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Publication No.: US09453903B2Publication Date: 2016-09-27
- Inventor: Ian S. Robinson
- Applicant: Raytheon Company
- Applicant Address: US MA Waltham
- Assignee: Raytheon Company
- Current Assignee: Raytheon Company
- Current Assignee Address: US MA Waltham
- Main IPC: G01S5/02
- IPC: G01S5/02 ; G01S19/39 ; B64G1/24 ; B64G1/36 ; G01S19/11 ; G01S19/48

Abstract:
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.
Public/Granted literature
- US20140354477A1 Satellite Orbital Determination (OD) Using Doppler and Kepler Orbital Elements Public/Granted day:2014-12-04
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