Classifications

• • H—ELECTRICITY
  • H04—ELECTRIC COMMUNICATION TECHNIQUE
  • H04B—TRANSMISSION
  • H04B7/00—Radio transmission systems, i.e. using radiation field
  • H04B7/14—Relay systems
  • H04B7/15—Active relay systems
  • H04B7/185—Space-based or airborne stations; Stations for satellite systems
  • H04B7/195—Non-synchronous stations

Definitions

• the invention relates to satellite communications, and, in particular, to a system and method for routing data to a ground station through a non-geostationary satellite system.
• Satellite communication systems transmit data to and receive data from users via radio-frequency communication links with movable (in a vehicle, airplane or ship, for example) or immovable ground stations.
• Such data can include voice, paging information, audio-visual information, facsimile data, and any other type of data or information.
• the first, existing conventional method of addressing and routing data or voice packets across a satellite constellation from one fixed ground station to another is to require the originating ground station to understand and tell the satellite constellation the proper route to take to get to the destination ground station.
• the originating ground station has to know which satellite is serving the destination ground station at all times. This usually requires a large amount of processing power in the originating ground station for calculating the exact location of all satellites in the constellation and for projecting the exact times that the destination ground station will be served by each satellite in the constellation.
• a large amount of bandwidth is required to communicate that information to the originating ground station every time the path to the destination ground station changes (as it will in a non-geostationary system).
• the second, existing conventional method of addressing and routing packets across a non-geostationary constellation is to require that each satellite in the constellation be able to track each destination ground station and translate that destination into address and routing information.
• This address and routing information changes as the non-geostationary constellation orbits the earth.
• This second conventional method requires a vast amount of processing power and storage in each of the satellite. Increased processing power and memory is directly proportional to increasing each satellite's weight and power requirements.
• FIG. 1 shows a satellite communication system according to a preferred embodiment of the present invention
• FIG. 2 shows an example of a relationship of an earth-based sector to a satellite footprint
• FIG. 3 shows a method of routing data from one ground station to another through a non-geostationary satellite system according to a preferred embodiment of the present invention.
• the present invention resolves the problem of addressing and routing packets of data or information through non-geostationary satellite constellation systems, including low-earth or medium-earth satellite constellations, or combinations thereof.
• This invention utilizes the concept of dividing the earth into sectors, assigning movable and immovable base stations and ground stations to those sectors, and routing packet data through the satellite constellation based on the way the non-geostationary satellite system covers the earth.
• a "satellite" as used throughout this description means a man- made object or vehicle which orbit the earth at non-geostationary altitudes (e.g., low-earth or medium-earth altitudes).
• a “constellation” means a number of satellites arranged in orbits for providing specified coverage (e.g., radio communication, remote sensing, etc.) of a portion, portions or all of the earth.
• a constellation typically includes multiple rings (or planes) of satellites and may have an equal number of satellites in each plane, although this is not essential.
• FIG. 1 shows a satellite communication system according to a preferred embodiment of the present invention.
• system 10 comprises a number of satellites 20, any number of ground stations 30, 31 and any number of base stations 40.
• communication system 10 including satellites 20, ground stations 30, 31 and base station 40 may be viewed as a network of nodes. All nodes of communication system 10 are or may be in data communication with other nodes of communication system 10 through communication links. In addition, all nodes of communication system 10 are or may be in data communication with other telephonic devices dispersed throughout the world through public switched telephone networks (PSTNs) and/or conventional terrestrial communication devices coupled to a PSTN through conventional terrestrial base stations.
• PSTNs public switched telephone networks
• the preferred embodiment of the present invention is applicable to space-based communication systems that assign particular regions on the earth to specific cells on the earth, and preferably to systems that move cells across the surface of the earth.
• satellite 20 is preferably part of a number of satellites in low-earth orbit around earth.
• satellite 20 can be a medium-earth orbit satellite.
• Satellite 20 can be in the same satellite network, or can be in different satellite networks, including for example, the IRIDIUM ® and/or the GLOBALSTAR ® networks. If they are in different satellite networks, one network can be designated as a primary satellite network, while the other satellite network can be designated as a secondary satellite network.
• Satellite 20 can be one of many satellites in at least one constellation of satellites orbiting earth.
• the present invention is also -4- applicable to space-based communication systems 10 having satellites 20 which orbit earth at any angle of inclination including polar, equatorial, inclined or other orbital patterns.
• the present invention is applicable to systems 10 where full coverage of the earth is not achieved (i.e., where there are "holes" in the communication coverage provided by the constellation) and to systems 10 where plural coverage of portions of the earth occur (i.e., more than one satellite is in view of a particular point on the earth's surface).
• Each satellite 20 communicates with other adjacent satellites 20 through cross-links in the preferred embodiment of the present invention.
• These cross-links form a backbone of space-based satellite communication system 10.
• a call or communication from one ground station located at any point on or near the surface of the earth may be routed through a satellite or a constellation of satellites to within range of substantially any other point on the surface of the earth.
• a communication may be routed down to a ground station (which is receiving the call) on or near the surface of the earth from another satellite 20.
• Ground stations 30, 31 may be located anywhere on the surface of earth or in the atmosphere above earth.
• Communication system 10 may accommodate any number of ground stations 30, 31.
• Ground stations 30, 31 are preferably communication devices capable of transmitting and receiving data.
• the data can of any type, including alphanumeric or numeric for example.
• ground stations 30, 31 can be customer premise equipment, adapted to transmit to and receive video transmissions from satellites 20.
• ground stations 30, 31 do not have to be mobile or moving, but can be fixed in one location for an extended period of time. How ground stations 30, 31 physically transmit data to and receive data from satellites 20 is well known to those of ordinary skill in the art.
• ground stations 30, 31 communicate with satellite 20 using a limited portion of the electromagnetic spectrum that is divided into numerous channels.
• the channels are preferably combinations of L-Band, K-Band and/or S-band frequency channels but may encompass Frequency Division Multiple Access (FDMA) and/or Time Division Multiple Access (TDMA) and/or -5-
• CDMA Code Division Multiple Access
• Base station 40 communicates with and controls satellites 20. There may be multiple base stations 40 located at different regions on the earth. For example, there may be one base station 40 located in Honolulu, another located in Los Angeles and another in Washington, D.C. Another example is to have separate base stations located in each country on the earth. Base stations 40 can provide satellite control commands to satellites 20 so that satellites 20 maintain their proper orbital position and perform other essential housekeeping tasks. Base stations 40 can be additionally responsible for receiving calling packet data, paging data or other types of information from satellite 20. How base stations 40 physically communicate with satellites 20 and/or ground stations 30 is well known to those of ordinary skill in the art. Base station 40 can additionally be connected to a PSTN.
• Base stations 40 provide certain basic services within satellite communication system 10. They provide control of access to the system for subscribers for whom a base station is "home", e.g., where information is stored about the subscribers, including information to authenticate the subscriber's identity and what services are available to the subscriber.
• the base stations 40 also provide system subscribers with access to PSTN(s), and it provides PSTN customers with access to system subscribers through the satellite network.
• FIG. 2 shows an example of a relationship of an earth-based sector to a satellite footprint. As shown in FIG. 2, each sector 50 is represented by a square although other shapes and sizes can be used as well. FIG. 2 shows twelve sectors in a three row by four column matrix. In the preferred embodiment, earth 52 is divided into less than 1000 sectors.
• Sector 50 is defined as a geographical area on earth 52 which is less than or equal to the projection of a single satellite antenna pattern 54 on the earth. Although antenna pattern 54 is shown as circles in FIG. 2, those of ordinary skill in the art know that antenna pattern 54 can have other shapes and sizes as well, including an elliptical shape, for example. Sector 50 has to be small enough to be completely or almost covered by a single satellite.
• Base station 40 is responsible for dividing earth into a number of regions, each region being distinct from another region, and for assigning a unique sector number to each of the regions.
• All ground stations are assigned to one sector 50.
• a ground station is assigned one of the sectors 50 upon installation by using various means well known to those of ordinary skill in the art, including referring to a latitude and longitude of where the ground station is going to be located on earth and setting the sector number of the ground terminal to the sector that corresponds to particular latitude and longitude.
• the particular latitude and longitude of where a ground terminal is located can be obtained from a Global Positioning System (GPS), for example. GPS is well known to those of ordinary skill in the art.
• GPS Global Positioning System
• FIG. 3 shows a method of routing data from one ground station to another through a non-geostationary satellite system according to a preferred embodiment of the present invention.
• method 100 is discussed in reference to routing a data packet between two ground stations, it is equally applicable for routing data packet or packets between a ground station and a base station, or between two base stations.
• ground stations are addressed by specifying an individual ground station identifier and a sector in which that ground station is located.
• Each satellite in the non-geostationary constellation tracks which satellite(s) can service which sectors at specific periods of time.
• the method determines a "most likely" serving satellite whereby all data packets for all ground stations in that sector will be sent to it.
• the most likely serving satellite determines if it is serving the destination ground station. If the most likely serving satellite is not serving the destination ground station, it will multicast that packet to each of its neighbor satellites. Each of those satellites attempt to serve the destination ground station.
• method 100 begins in step 102 when an originating ground station ("OGS") transmits a packet to a satellite serving the sector where the OGS is located.
• OGS originating ground station
• a packet is addressed to the serving satellite by specifying an address which comprises a sector of where the destination ground station (“DGS”) is located and a sector unique ID of the DGS.
• DGS destination ground station
• the sector unique ID identifies the DGS from other DGS's.
• the satellite serving the OGS checks the address of the packet sent by the OGS and determines in step 104 whether it is the most likely satellite to be serving the destination sector. The determination can be as simple as checking the sector of the DGS sent in the address of the packet against a table of sectors stored in the satellite that list what sectors are currently being serviced by the satellite. There are other ways of making this determination which are well known to those of ordinary skill in the art. If the satellite determines in step 104 that it is not the most likely satellite to be serving the DGS, the satellite determines in step 106 what satellite is the most likely satellite to be serving that sector.
• the determination of what satellite is the most likely satellite can be based on a comparison between the sector of the DGS (contained in the address of the packet) with a table which associates each sector with a particular satellite. If the current satellite is in direct communication with the most likely satellite, the current satellite transmits in step 107 the packet to the most likely satellite. However, if the current satellite is not in direct communication with the most likely satellite, the current satellite has to determine what intervening satellite should receive the packet. The "next satellite" refers to the intervening satellite that should receive the packet. Once the determination of what intervening satellite should receive the packet, the current satellite transmits in step 107 the packet to the next satellite.
• step 104 determines whether it is the most likely satellite to serve the sector of the DGS.
• steps 104 and 106 are repeated until a satellite determines that it is the most likely satellite to be serving the destination sector of the DGS.
• a packet can pass through many other intervening satellites, each one checking to see if it is the most likely satellite to serve the destination sector. Each one forwards the packet until the most likely satellite is reached. -8-
• step 108 determines whether it is still actually serving the DGS. This determination performed by step 108 is needed because the satellites are always moving in orbit around the earth, and by the time the packet reaches the most likely satellite, it has stopped communicating with the DGS.
• the most likely satellite determines that it is still serving the DGS in step 108, the most likely satellite transmits in step 110 the packet to the DGS.
• the transmission by the most likely satellite occurs on a beam and frequency to which the DGS is tuned.
• the most likely satellite transmits the packet to all neighboring satellites in step 112.
• a neighboring satellite is one in which the satellite has a direct connection (via a cross-link). There is a strong possibility that one of the neighboring satellites is serving the sector of where the DGS is located. If one of the neighboring satellites determines in step 114 that it is serving the sector of where the DGS is located, the packet is transmited in step 110 by the other satellite to the DGS. Subsequent to step 110, method 100 ends. Otherwise, the packet is discarded in step 116, and method 100 ends. Method 100 ensures that the packets will find its destination and reach the DGS even if the most likely satellite changes while the packet is being routed.
• Another advantage of the invention is that the complexity of the ground stations is reduced by allowing the grounds stations to use a fixed, earth-based sector addressing scheme to locate and find any ground station. The fact that the satellites are orbiting the earth is transparent to the ground stations. Thus, the ground stations do not have to keep satellite ephemeris data in order to send packets to destination ground stations. This significantly reduces the bandwidth (constantly receiving satellite ephemeris data), processing power (projecting future satellite ephemeris), and storage (storing projected satellite ephemeris) in the ground stations.
• Yet another advantage of the invention is that routing on the satellite is simplified in comparison to other fixed earth addressing schemes. Since the address contains the destination sector of the DGS, the satellite performs a quick look-up in a table of less than 1000 sectors (as opposed to possible millions of ground stations) to determine if the packet is meant for this satellite. Only if the packet is destined for a sector being served by that satellite does the satellite have to inspect the entire address. This address sectorization reduces storage requirements, required processing power, and routing delay on the satellite.
• conventional routing methods required the originating ground station to know the satellite that is serving the destination ground station. In those schemes, each time a ground station's communication links are handed from one satellite to the next, signaling had to be used to inform the originating ground station that a handoff had occurred.
• This invention eliminated the need for the originating ground station to know the destination satellite, thus preserving this bandwidth for traffic use.

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• Engineering & Computer Science (AREA)
• Physics & Mathematics (AREA)
• Astronomy & Astrophysics (AREA)
• Aviation & Aerospace Engineering (AREA)
• General Physics & Mathematics (AREA)
• Computer Networks & Wireless Communication (AREA)
• Signal Processing (AREA)
• Radio Relay Systems (AREA)
• Mobile Radio Communication Systems (AREA)

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• 1998
  • 1998-03-27 US US09/049,533 patent/US6173176B1/en not_active Expired - Lifetime
• 1999
  • 1999-03-22 GB GB9927636A patent/GB2342540B/en not_active Expired - Fee Related
  • 1999-03-22 CA CA002289514A patent/CA2289514A1/en not_active Abandoned
  • 1999-03-22 JP JP54949899A patent/JP2002500854A/ja not_active Withdrawn
  • 1999-03-22 WO PCT/US1999/006305 patent/WO1999050976A1/en unknown
  • 1999-03-26 FR FR9903799A patent/FR2776867A1/fr active Pending
  • 1999-11-29 SE SE9904308A patent/SE9904308L/ not_active Application Discontinuation

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