发明名称 Method and articles of manufacture for time-space-position-information (TSPI)
摘要 A method for time-space-position-information (TSPI) for at least one air-based platform in a flight test includes providing a system having components to collect TSPI. The system, which includes an air-based platform, is initialized and a flight test is started. The system is remotely monitored to determine system diagnostics and, when system problems are diagnosed, they are fixed by remote configuration or manual repair. TSPI data is received with ground-based receiver nodes through a wireless data link signal transmitted from a dedicated on board transmitter on the air-based platform. The dedicated on board transmitter uses a known transmitter signal waveform. The ground-based receiver nodes match an internally generated signal waveform to the known transmitter signal waveform to measure time of arrival. The TSPI data is collected and sent to a ground processing station. The TSPI data is processed with the ground processing station. The system components and TSPI data are collected. The TSPI data is produced as output.
申请公布号 US9070236(B1) 申请公布日期 2015.06.30
申请号 US201314093322 申请日期 2013.11.29
申请人 The United States of America as Represented by the Secretary of the Navy 发明人 DiEsposti Raymond S.
分类号 G07C5/00;G07C5/08 主分类号 G07C5/00
代理机构 代理人 Saunders James M.
主权项 1. A method to determine time-space-position-information for at least one air-based platform in a flight test, comprising: (a) providing a system having components to collect time-space-position-information (TSPI), said system components, comprising: at least one air-based platform having an on-board navigation system, a dedicated on-board transmitter, and a dedicated on-board receiver, wherein said on-board navigation system is configured for computing time-space-position-information (TSPI) and providing a wireless data link between said at least one air-based platform and the ground, wherein said dedicated on-board transmitter and said dedicated on-board receiver are configured for transmitting and receiving signals with navigation information, control commands, and messages through said wireless data link, wherein said at least one air-based platform is selected from the group of air-based platforms consisting of air vehicles, rockets, launch vehicles, aerostats, space vehicles, and precision guided munitions;a plurality of ground-based components in communication with said at least one air-based platform; (b) initializing said system for a flight test, said initializing task, comprising: determining whether said flight test is a GPS-denied test; when said flight test is a GPS-denied test, remotely initializing and configuring said system to operate without GPS; andwhen said flight test is not a GPS-denied test, remotely initializing and configuring said system to operate using GPS; (c) starting said flight test; (d) remotely monitoring said system to determine system diagnostics, said system diagnostics indicating system health; when it is determined that said system is not functioning properly, diagnosing system problem;fixing system problem by remote reconfiguration or manual repair and iterating through task (d) until said system is functioning properly; (e) receiving TSPI data with a plurality of ground-based receiver nodes through a wireless data link signal transmitted from said dedicated on board transmitter on said at least one air-based platform, wherein said dedicated on board transmitter uses a known transmitter signal waveform, wherein said plurality of ground-based receiver nodes match an internally generated signal waveform to said known transmitter signal waveform to measure time of arrival (TOA) and frequency of arrival (FOA); (f) collecting said TSPI data when said system is determined to be functioning properly; (g) sending TSPI data to a ground processing station; (h) processing said TSPI data with said ground processing station and geolocating said on-board transmitter using emitter signal geolocating techniques, said emitter signal geolocating techniques selected from the group of emitter signal geolocating techniques consisting of time of arrival (TOA), frequency of arrival (FOA), time difference of arrival (TDOA), and frequency difference of arrival (FDOA); (i) determining whether said flight test is complete; when it is determined that said flight test is not complete, iterating through tasks (d) through (i), until it is determined that said flight test is complete; (j) collecting said system components and said TSPI data; and (k) outputting said TSPI data in a tangible medium.
地址 Washington DC US