SWITCHING METHODS FOR SATELLITE COMMUNICATION SYSTEM

Abstract: The Switching Methods for a Satellite Communication System overcome the limitations encountered by conventional packet switching using virtual circuits. The present invention utilizes a ''datagram'' approach that routes every packet (22) conveyed by the system independently at every node in the network. The packets (22) are directed along an optimized pathway through the network by a fast packet switch (38) that directs traffic based on instructions from an adaptive routing processor (14) that continuously runs an adaptive routing algorithm (16). This adaptive routing processor (14) works together with an input packet processor (28) and a routing cache memory (20) to monitor the rapidly changing topology of each satellite (S) in the constellation and the distribution of traffic among its nodes and links. The input packet processor (28) functions like a gatekeeper or guide that extracts the destination node address (32) from each packet (22) and uses it to access routing information stored in the routing cache memory (20).

Description: Switching Methods for Satellite Communication System CROSS-REFERENCES TO RELATED PATENT APPLICAΗONS The present patent application is related to the following commonly-owned and commonly- assigned pending patent applications filed on October 28, 1991, November 8, 1991, June 6, 1992, July 16, 1992 and August 18, 1992: Satellite Communication System by Edward Fenton Tuck et al., assigned United States Serial Number 07/783,754; Method of Conducting a Telecommunications Business Implemented on a Computerby Edward Fenton Tuck, assigned United States Serial Number 07/895,295; Terrestrial Antennas for Satellite Communication System by Asu Ram Jha, assigned United States Serial Number 07/790,273; Beam Compensation Methods for Satellite Communication System by David Palmer Patterson and Mark Alan Sturza, assigned United States Serial Number 07/790,318; Spacecraft Antennas & Beam Steering Methods for Satellite Communication System by Douglas Gene Lockie, assigned United States Serial Number 07/790,271; Spacecraft Intersatellite Link for Satellite Communication System by Douglas Gene Lockie et al, assigned United States Serial Number 07/915,172; and Spacecraft Designs for Satellite Communication System by James R. Stuart, assigned United States Serial Number 07/931,625. The specifications of the patent appUcations listed above are hereby incorporated by reference. DESCRIPTION OF THE INVENTION TECHNICAL FIELD The present invention relates to the field of satellite communications. More particularly, this invention provides a novel fast packet switching method for a network having a rapidly changing topology. Each packet moved through the network is routed independently at each network node along an optimum route that is selected by the switch. BACKGROUND ART A portion of long-distance telephone traffic is relayed by satellite networks. Some of the radio signals that convey these telephone calls are grouped into sequences of digital bits called "packets." In conventional packet networks are carried to their destination through a pathway called a "virtual circuit." A virtual circuit is a route through a network from an origin to a destination that is established at the initiation of a call, and then is released when the call is terminated. The virtual circuit defines a path that includes nodes and links in the network that are used by all the packets associated with the virtual circuit. The packets arrive at their destinations by following instructions or maps that are generated at the origin of the call. Any change in network topology after the call is initiated and the packet itinerary is generated, such as the failure of a node or link, causes a discontinuity in the virtual circuit. When the virtual circuit is disturbed, the packet's itinerary is no longer valid, and the call is disconnected. Re-establishing a broken call by generating a new virtual circuit every time a failure occurs is a lengthy, inefficient and expensive process. Conventional systems that employ packets that are switched through virtual circuits are capable of providing reliable communications service in networks that are static. If the nodes and the links connecting the nodes are dynamic, the use of packets that follow directions along a fixed itinerary in a virtual circuit that was mapped at the origin of the call becomes impractical. A satellite communications system that utilizes satellites in geosynchronous orbit is generally a static system, since the spacecraft do not change position appreciably relative to relay stations on the ground beneath them. Geosynchronous satellites, however, operate in very high 22,000 mile orbits, and the propagation delays inherent in conveying signals over a nearly 50,000 mile round-trip are not acceptable for many telephone environments. This intolerably long transit delay is only one of several reasons that militate against the use of high Earth orbit geostationary satellites for a world-wide communications system. One alternative to a geosynchronous system is a constellation of satellites operating in low Earth orbits. In the past, this alternative was not viable, because conventional switching methods that employ packets routed through static virtual circuits using itineraries generated at the origin of a call can not cope with the rapidly changing topology of a low Earth orbit network. No single public communications network is presently capable of offering continuous global service to a wide variety of customers using mobile, portable, and fixed terminals. The problem of providing an economically viable, 24-hour, world-wide network for voice, data, and video has presented a major challenge to the communications business. The development of a fast packet switch which could direct packetized call traffic through a constantly changing network would constitute a major technological advance and would satisfy a long felt need within the electronics and telephone industries. DISCLOSURE OF THE INVENΗON The Switching Methods for a Satellite Communication System overcome the limitations encountered by conventional packet switching using virtual circuits. The present invention utilizes a "datagram" approach that routes every packet conveyed by the system independently at every node in the network. The packets are directed along an optimized pathway through the network by a fast packet switch that directs traffic based on instructions from a microprocessor that continuously runs an adaptive routing algorithm. This microprocessor uses orbital position information generated aboard each spacecraft to monitor the rapidly changing topology of the constellation and the distribution of traffic among its nodes and links. The present invention is a vital element of a novel Satellite Communication System, which is described in a related patent application that is referred to above. The present invention comprises a self-routing fast packet switch, an input packet processor, a routing cache memory, and an adaptive routing processor. The input packet processor functions like a gatekeeper or guide that extracts the destination node address from each packet and uses it to access routing information stored in the routing cache memory. The adaptive routing processor constantly updates the routing cache memory so each satellite has an accurate "knowledge" of the whereabouts of all its neighbors, and of the expected packet delay from adjacent nodes to all possible destination nodes. Based upon this position and expected delay information, the adaptive routing processor selects the best pathway from a particular satellite to a single neighboring satellite, and the packet is then moved through internal switch circuitry onboard the satellite on its way to other spacecraft in its journey to some eventual destination on Earth. The fast packet switch of the present invention optimizes the utilization of the network facilities and minimizes transmission delays and variances of transmission delays. By precalculating the optimal route for each packet one step at a time at each satellite, the amount of time required to process individual packets is greatly reduced. An appreciation of other aims and objectives of the present invention and a more complete and comprehensive understanding of this invention may be achieved by studying the following description of a preferred embodiment and by referring to the accompanying drawings. BRIEF DESCRIPπON OF THE DRAWINGS Figure 1 is a flowchart that shows the generalized fast packet switch. Figure 2 presents a block diagram of a satellite switch node that includes the fast packet switch. Figure 3 is a schematic illustration of a 32 by 1 packet priority multiplexor. Figure 4 reveals a block diagram of a fast packet switch. Figure 5 shows a 1 by 32 self-routing switch module. Figure 6 is a schematic diagram of node hardware architecture. Figure 7 depicts a routing process. Figure 8 supplies a flowchart that explains dynamic packet routing. Figure 9 is a chart which reveals the relationships among terminals, satellites, databases, feature processors, and gateways. Figure 10 is a schematic diagram of an output module. Figure 11 exhibits the function of a concentrator circuit. Figure 12 presents a schematic diagram of switching architecture. Figure 13 supplies a schematic diagram of a packet structure. Figure 14 discloses the lines of communication between the packet switch and its communication links to the world outside each satellite. Figure 15 furnishes a view of internal communications centered on an FDDI token ring. Figure 16 is a schematic diagram of a packed switch and input output processors coupled together by an FDDI token ring. Figure 17 shows GSL modems and a GSL switching matrix. Figure 18 provides a diagram of switching logic circuitry. Figure 19 is a schematic diagram of an FDDI ring and its connections to input output processor (IOP) units. Figure 20 is a block diagram that illustrates the interface between receive and transmit modems and the fast packet switch. Figure 21 reveals some aspects of the packet routing process. Figure 22 depicts the aπangement of input packet processors (IPP) and an IPP common control unit. Figure 23 is a schematic diagram of an IPP 4-stage pipeline. Figure 24 furnishes an overview of the routing process that generates a set of time delay vectors to produce an optimal link tag for each packet. Figure 25 shows how packets are received from the packet switch and then sorted in cell and channel buffers to await shipment to satellite antennas. Figure 26 portrays a message transport system associated with the packet switch. Figure 27 is a schematic diagram of a 128 by 128 switch. Figure 28 is a schematic diagram of a single switching cell. BEST MODE FOR CARRYING OUT THE INVENΗON Figure 1 is a flow chart 10 that explains the switching process as it occurs on each satellite S in the orbiting constellation. Orbital position information 12 is fed to an adaptive routing processor 14 which runs an adaptive routing algorithm (ARA) 16. The ARA 16 constantly monitors the changing locations of all the spacecraft S in the constellation, and also keeps track of communications traffic congestion among the links and nodes of the system. The adaptive routing processor 14 produces an output called "Next-node-in-path-to-destination" 18. As the name implies, this output 18 contains information and provides instructions for moving communications data through the network one node at a time. Each satellite and gateway in the network are treated as "nodes", and every transmission between any two "nodes" is treated as a "link". Transmissions from nodes to terminals also occur over a link. Packets 22 generated by a packetizing circuit (not shown) arrive at one of the satellites S from a portable (P), mobile (M) or fixed (F) terminal or gateway (G) or from another satellite S. Packeting circuits may include analog-to-digital converters that are well known in the electronic arts which translate audio signals to streams of digital bits. Each packet 22 comprises a string of one's and zero's and is divided into two general sections called a header 24 and a payload 26. The payload 26 carries the "message" or substance of the communicated information conveyed by the packet 22. The header 24 includes the packet's destination address, and information called a destination node 32, which refers more particularly to the location in the network where the packet must be delivered. An input packet processor 28 receives an asynchronous sequence of packets in a serial transmission format. Each packet 22 contains information in its header section 24 that enables circuitry aboard the satellites S to route the packets 22. The input packet processor 28 extracts the destination node information from each packet 22 and forwards the destination node 32 as an input to a routing cache memory 20. This memory 20 is also the recipient of next-node-in- path-to-destination output 18 produced by the adaptive routing processor 14. Since the routing cache memory 20 is used by more than one input packet processor 28, a time-sequencer or multiple cache memories can be used to eliminate contention problems that occur when more than one input packet processor 28 seeks the services of the cache 20. The input packet processor 28 receives a next node routing tag 30 from the routing cache memory 20 prepends the tag 30 to the processed packet 34, and forwards the processed packet 34 to a fast packet switch 38. The switch 38 receives the processed packet 34 through one of its many input ports 36, and conveys it to one of many multi-stage self-routing switch sections (MSSRSS) within it. The tag 30 is read by an MSSRSS, and the MSSRSS automatically routes it to an asynchronous packet multiplexing section (APMS). The multiplexing section multiplexes the packets 34 received in parallel from various input ports 36 into a serial output stream at one of its output ports 40. Figure 2 presents a block diagram of a satellite switch node 42. One fast packet switch 38 is shown in the upper portion of the diagram, and receives signals from a series of circuit modules 44 and 52. Module 44 includes a receiver 46 coupled to receive antennas (not shown in Figure 2), a demodulator 48, and a bit/packet synchronizer 50. Module 52 provides input packet control, and comprises circuits for error detection 54, packet tagging 56, local cache access 58 and network cache access 60. The series of input packet control modules 52 are also connected to control complex 62 through a local routing cache 76 and a local routing and handover processor 74. Another link to the input packet control modules 52 are coupled to the control complex 62 through a network routing cache 80 and a network management and routing processor 78. The control complex 62 is an array of circuit stages that include a signalling and call control processor 64, a test and maintenance processor 66, a system control and reload processor 68, a billing and traffic processor 70 and a satellite ephemerides processor 72. The control complex 62 is coupled to a communications processor 82, a spare processor 84 and a beam steering processor 86, which is connected to output packet control modules 90 and 96. Modules 90 comprise circuits that keep track of path history 92 and that are responsible for error encoding 94. Modules 96 include packet framing circuits 98, modulators 100 and transmitters 102 connected to transmit antennas (not shown in Figure 2). Figure 3 supplies a schematic illustration of a 32 by 1 packet priority multiplexor 104. Serial input signals 106 are fed to the multiplexor 104 at the rate of 150 megabits per second (MBITS) through a series of serial-to-parallel (S P) converters 108. The S/P converters 108 are coupled to first-in, first-out (FIFO) buffering circuits 110, which are also connected to status and control (S&C) circuits 112. All the S&C circuits 112 are linked to FIFO scanning and control logic circuitry 114 and an output queue status stage 116. An eight bit parallel bus 117 receives the output of the FIFO circuits 110, and are conveyed to a priority router 118, 8 by 16K low and high priority FIFO circuits 120 and 122, and through a parallel-to-serial converter (P/S) 124 to provide a 150 MBITS serial output 126. Figure 4 is a block diagram 128 which reveals the details of a fast packet switch 38. Serial inputs 130 are transported into the switch 38 via a series of 1 x 32 self-routing switch modules 132 that are, in turn, associated with a series of 32 x 1 asynchronous packet multiplexors 134. Figure 5 is a schematic diagram 136 that shows the details of the 1 x 32 self-routing switch module 132 illustrated in Figure 4. Packets 22 having headers 24 and payloads 26 are fed into the module 132 at the rate of 150 MBITS. The packet 22 comprises a string of ones and zeroes, and includes a priority flag, a routing tag and an error flag. A series of self-routing cells 138 read the bits in the header 24, and direct routed packets 142 with their payloads of data 26 to the output side 140 of the module 132. Figure 6 is a schematic diagram of node hardware architecture 200 employed by the present invention. A common control stage 202 aboard each spacecraft is capable of conveying internode messages 204 and 206 to receivers 208 and transmitters 210 which communicate with the other satellites S in the constellation. The common control stage 202 is also linked to a fast packet switch 38, which forwards routed packets 22 to other satellites S, to gateways G or to subscribers using portable P, mobile M or fixed F terminals. The routing process is illustrated in the flow diagram 214 shown in Figure 7. Service demand 216 from subscribers 218 situated around the world prompt the routing algorithm 16 to determine optimum pathways for call traffic using routing tables 220 and other local processes 222. Figure 8 exhibits dynamic packet routing in diagram 224. The router 226 uses entries stored in routing tables 220 to instruct packet routers 228 how to process packets 22 to a sorting network 230 and associated transmitters 232. Packets 22 generated at traffic sources are switched through the network in a store-and-forward fashion. The router 226 at each hop forwards the packet to the next hop, minimizing the packet end-to-end delay which the packet experiences in its trip from the source to the destination. The decision of how to forward a packet 22 is determined by each hop independently with no a-priori or static route determination. Routing decisions are based on the latest information available to the router at the switching hop, and reflect dynamic global network considerations as well as the local node considerations. In the one of the preferred embodiments, both satellites S and gateways G possess routing capabilities, so the term "node" is used to refer both to satellites and to gateways. A gateway is treated simply as a stationary satellite. The term "routing" not only includes the process of directing each packet at each node, but embraces the related operations of controlling traffic flow, overloads and congestion and optimizing traffic distribution. Figure 9 presents a schematic depiction 233 of the transmission between a portable P, mobile M or fixed F terminal and several satellites S in the orbiting constellation 234. A number of satellites S may be involved in routing the call from the terminal P, M or F to its destination at a gateway G. In this case, the gateway G is connected to a public switched telephone network (PSTN) 238. During the call routing process, some of the satellites S may consult with a subscriber database 235, feature processors 236 or a routing database 237. A block diagram of an output module 240 is revealed in Figure 10. An input 241 is conveyed into a fiber optic receiver 243 which is coupled to an input output module (IOM) that is linked to a fiber distributed data interface (FDDI) 242. Signals from the receiver 243 flow into a packet decoder 244, and then are split into separate pathways 245 and 246 for traffic from fixed and mobile terminals. Supercell decoders 247 pick a supercell as a route for each packet 22, and a series of thirty-two channel decoder stages 248 for both the fixed terminal traffic and mobile terminal traffic select channel assignments for the packets 22 which are sent to transmit encoders 249 (not shown in this Figure). Figure 11 furnishes a schematic diagram 250 of a circuit stage called a 7:1 concentrator 252. This device cuts down the number of ports on the fast packet switch 38 by substituting a relatively small number of high speed ports for a relatively large number of low speed ports. The concentrator 252 comprises statistical multiplexors, and distributes traffic more evenly among the links in the network. A group of receivers labeled 254 and 256 represent traffic handled by two sets of thirty- two receivers for mobile and fixed terminal calls. The seven-to-one concentrator 252 converts an input rate 258 of 24.480 Mbits per second to 3.544 Mb/s. The concentrator 252 is coupled to a series of transmitters 260 and to an input output module (IOM) 264 central processing unit (CPU). The IOM CPU 264 is also linked to the FDDI ring 242 through an FDDI server 262. Figure 12 presents a schematic illustration 266 that shows the details of the environment of the fast packet switch 38. Packets 22 flow into a series of forty-two input module multiplexors (IM MUX 1/42 - 4242) 268 coupled to concentrator 252, and then over 170Mb links 270 to an array of input packet processors (DPP) 28. Packets 22 from gateway satellite links (GSL) 274, inter-satellite links (ISL) and mobile terminal satellite links (MTS) 278 are also received by the IPP array 28. Packets from the B?Ps 28 are forwarded to switch 38, where traffic from the input modules 268 is fed to an array of forty-two facility multiplexors (FACEL MUX 1/42 - 42/42) 280. Output from the facility multiplexors 280 is conveyed to output module supercell and cell demultiplexors (OM DEMUX 1/42 - 42/42) 282. Call traffic bound for gateways G, other satellites S, and mobile terminals M exit the switch to links labeled 288, 290 and 291 respectively. Figure 13 reveals the structure of packets 22 which are conveyed through the network. In the preferred embodiment, all packets 22 conveyed through the network are 512 bits long. The first portion of the packet is a header 24 comprising 80 bits. The header 24 is a collection of control fields that define the packet priority and type and contain routing information. A routing field within the header 24 includes a destination field that contains a destination node and a specific call/delivery identification within the destination node. A 416 bit payload and a 16 bit cyclic redundancy check (CRC) accompany the header. The payload 26 carries the substance of the message which the packet transports, and the CRC is used to detect errors. The structure recited above is used as a basis for all of the discussion and examples which appear in this document. Figures 14 and 15 furnish schematic representations 292 and 310 of the lines of communication between the fast packet switch 38, the FDDI token ring 242 and links to the world outside each spacecraft S. In both figures, a central control unit 294 that includes a central processor 298 and a message transport unit 296 coordinate the flow of signals from gateways G over gateway satellite links (GSL) 300, inter-satellite links (ISL) 302, fixed terminal links (FTL) 304 and mobile terminal links (MTL) 306. A multiple access controller 308 oversees signals conveyed to and received from each satellite's antennas. The relationship among the fast packet switch 38 and a series of input output packet processor (IOP) units 314 are illustrated in a schematic depiction 312 provided by Figure 16. Chart 316 in Figure 17 explains how traffic from gateways G must be processed through modems 318 and a switching matrix 320 before it is received by the IPP array 28 and the fast packet switch 38. Figure 18 offers a schematic diagram 322 which supplies a detailed view of a high level representation of a portion of the self-routing network within the fast packet switch 38 that routes packets 22 by examining bits in the tag added by the output processor units. A decoder 324 works with routing elements 326 coupled together in an array to perform the packet sorting procedure. Figure 19 supplies a schematic layout 328 which indicates the deployment of input output processor units 314 on the FDDI ring 242. Coaxial lines 329 and 330 convey radio frequency (RF) signals to and from the ring 242. The relationship among transmit and receive modems 334, input packet processor units 28, and output packet processors 314 is depicted in the block diagram 332 found in Figure 20. Figure 21 is a flow chart 336 that explains the flow of packets 22 to the switch 38. A central processing unit CPU 338 manages signals passing to and from the FDDI ring 242 through an FDDI server 340. Packets 22 are checked for errors by a CRC checker. Supercell, cell and channel assignments are supplied by a Call ID map 341, and are added to the header 24 of each packet 22. Routing instructions are also added to the header of the packet 22 after being determined by the cooperative action of the routing algorithm 16 and the routing tables 220. Figure 22 reveals the association of the input packet processor units (IPP) 28 and an IPP common control unit 343, while an IPP four stage pipeline 344 is shown in Figure 23. Figure 24 furnishes a flow chart 345 that explains the general process performed aboard each satellite to produce routing instructions. The router 226 onboard each satellite or node (n) generates a local estimate of the delay that would be encountered in transmitting a packet 22 to any other node (x). These delays are computed for each of its links 1, 2,...,L to other satellites, gateways and terminals. The delay realized by a packet in transit between two nodes in the network n and x over a particular link 1 is given by the expression: Algorithm 1: D(n, x, 1) = Tp(l) + Tq(l) + ND1(1*, x) The quantity Tp(l) is the current propagation delay for a link 1 which connects a local node n to the neighbor node terminating 1 at its remote edge. This neighbor is designated 1* (the symbol * is used to mean "the successor of)". Tp(l) varies with time as the distance between n and 1* changes with satellite movement. Tq(l) is the current link queuing delay consisting of two components, Tb and Ts. Tb represents the time spent by a packet in a buffer waiting for all the packets ahead of it to be transmitted. Ts is the actual packet transmission time once it gets to the queue head (called the service time). Ts is a function of the packet length and the link transmission bandwidth. The variable ND(1*, x) is the delay reported by neighbor 1* to n stating the least delay from itself (from neighbor node 1*) to destination node x. The router in n maintains a table ND1(1*, x) for each of its links, and reflects the most recent delay reported by neighbor 1* to each destination x. The terms Tp and Tq are derived by node n from local information, whereas the term NDl(l*,x) represents the distributed term. From the routers' viewpoint, if load control issues are ignored, the optimal link from n to destination node x is that link 1 for which D(n, x, 1) is lowest. The actual link used by n to forward packets to x is not always the optimal Unk. If objectives concerning traffic load distribution are factored into the decision, another Unk may be chosen. In flowchart 345 shown in Figure 24, the quantities Td, Tp and Tq are conveyed from the router map 346 within the router 226 and are processed by an optimal link select sequencer 347 to produce an optimal link tag that is used to route each packet 22. Figure 26 contains a flow diagram 358 that includes a message transport system 360. Packets 22 can be grouped into two general categories, those carrying user data comprising voice, video, digital data, etc.; and those carrying control messages that are used in network administration and control functions. Packets 22 passing through satellite nodes on their way to their final destinations may contain user data or control messages. If a particular packet 22 contains a control message for a satellite, it is delivered to the message transport system (MTS) 360. The MTS 360 communicates with internal circuitry and the outside world over the FDDI token ring 242. Figure 25 is a flowchart 348 which depicts the transit of a packet 22 from the output port 40 of switch 38 to transmission equipment. Packets 22 carrying cell and channel assignments and terminal packet indicator information 350 are fed to a cell decoder 352 which forwards each packet 22 to one of sixteen cell buffers 354 depending on the cell assignment carried in the packet header 24. Each cell buffer 354 contains a channel sorter 355 which sorts each packet by the channel to which it has been assigned. Three hundred and sixty channel buffers 356 within each ceU buffer 354 hold packets until the appropriate transmission time arrives, and then the sorted packets are emitted from the buffers 354 to RF modulators and, eventually, the satellite antennas. Figure 27 exhibits the pathways within a 128 x 128 switch 362, while Figure 28 is a schematic diagram of a single switching cell 364. CONCLUSION Although the present invention has been described in detail with reference to a particular preferred embodiment, persons possessing ordinary skill in the art to which this invention pertains will appreciate that various modifications and enhancements may be made without departing from the spirit and scope of the claims that follow. The various orbital parameters and sateUite population and configuration statistics that have been disclosed above are intended to educate the reader about one preferred embodiment, and are not intended to constrain the limits of the invention or the scope of the claims. The List of Reference Characters which foUows is intended to provide the reader with a convenient means of identifying elements of the invention in the specification and drawings. This list is not intended to delineate or narrow the scope of the claims. INDUSTRIAL APPLICABILITY The Switching Methods for Satellite Communication System described above wiU help to overcome the limits that circumscribe the performance and potential of existing telephone systems. The system is capable of offering continuous voice, data and video service to customers across the globe on the land, on the sea, or in the air. Instead of merely improving upon or expanding existing land-based systems, the system bypasses centralized terrestrial switching hardware by placing aU the intelligence of the network in orbit. Unlike conventional hierarchical networks, which are linked together by a complex web of wires, cables, glass fibers, and microwave repeaters that are very expensive to bmld and maintain, the present invention Uberates the true communications potential of existing land-based networks by routing signals through spacecraft in low Earth orbit. The present invention wiU revolutionize the telecommunications industry, and offer a wide spectrum of services and industrial opportunities around the world. LIST OF REFERENCE CHARACTERS 10 Flow chart of switching process 12 Orbital position information 14 Adaptive routing processor 16 Adaptive routing algorithm 18 "Next-node-in-path-to-destination" output 20 Routing cache memory 22 Packets 24 Header 26 Payload 28 Input packet processor 30 Next node routing tag 32 Destination node 34 Processed packet 36 Input ports 38 Fast packet switch 40 Output port 42 SateUite switch node 44 Circuit modules 46 Receiver 48 Demodulator 50 Bit/packet synchronizer 52 Input packet control modules 54 Error detection circuits 56 Packet tagging circuits 58 Local cache access 60 Network cache access 62 Control complex 64 CaU control processor 66 Maintenance processor 200 Node hardware architecture 202 Common control stage 204 Internode messages 206 Internode messages 208 Receivers 210 Transmitters 214 Routing process 216 Service demand 218 Subscribers 220 Routing tables 222 Local processes 224 Dynamic packet routing method 226 Router 228 Packet routers 230 Sorting network 232 Transmitters 233 Schematic diagram of caU routing through consteUation 234 SateUite consteUation 235 Subscriber database 236 Feature processor 237 Routing database 238 PubUc switched telephone network 240 Output module 241 Output module input 242 FDDI 243 Fiber optic receiver 244 Packet decoder 245 Fixed terminal traffic 246 MobUe terminal traffic 247 SuperceU decoder 248 Channel decoder stages 249 Output to transmit encoders 250 Diagram showing concentrator environment 252 Concentrator circuit 254 Receivers 256 Receivers 258 Concentrator input rates 260 Transmitters

Claims: CLAIMS What is claimed is: 1. An apparatus for communicating among a pluraUty of portable (P), mobUe (M) and fixed (F) terminals, gateways (G) and satellites (S) comprising: a pluraUty of sateUites (S) in Earth orbit; each of said pluraUty of sateUites (S) being capable of receiving a pluraUty of packets (22) from one of said pluraUty of portable, mobile and fixed terminals, gateways and other of said pluraUty of sateUites in Earth orbit; said pluraUty of packets (22) each including a header (24) and a payload (26); said header (24) including a destination address; said payload (26) including a message; each of said pluraUty of sateUites (S) including a fast packet switch (38); said fast packet switch (38) being capable of extracting said destination address from said header (24); each of said fast packet switches (38) also being capable of routing each of said pluraUty of packets (22) independently based upon orbital position information (12) generated onboard each of said pluraUty of sateUites (S) to one of said pluraUty of portable (P), mobfle (M) and fixed (F) terminals, gateways (G) and other sateUites (S) in Earth orbit. 2. A method of communicating among a pluraUty of portable (P), mobUe (M) and fixed (F) terminals, gateways (G) and sateUites (S) in Earth orbit comprising the steps of: receiving a packet (22) aboard one of said pluraUty of sateUites (S) in Earth orbit from one of said pluraUty of portable, mobile and fixed terminals, gateways and other sateUites in Earth orbit; said packet (22) including a header (24) and a payload (26); said header (24) including a destination address; said payload (26) including a message; extracting said destination address from said header (24); routing said packet (22) independently based upon orbital position information generated onboard said sateUite (S) to one of said pluraUty of portable (P), mobile (M) and fixed (F) terminals, gateways (G) and other sateUites (S) in Earth orbit. 3. A apparatus for directing a communications signal onboard a pluraUty of sateUites (S) in Earth orbit comprising: an adaptive routing processor (14) which includes and continuously runs an adaptive routing algorithm (16); said adaptive routing algorithm (16) capable of using orbital position information (12) concerning said pluraUty of sateUites (S) in Earth orbit to produce a next- node-in-path-to-destination output (18); a routing cache memory (20) coupled to said adaptive routing processor (14); said routing cache memory (20) being capable of receiving said next-node-in-path-to-destination output (18) from said adaptive routing processor (14) and also being capable of producing a next node routing tag (30); an input packet processor (28); said input packet processor (28) being connected to said routing cache memory (20); said input packet processor (28) being capable of receiving a packet (22); said packet (22) including a header (24); a payload (26); and said header (24) including a destination address; said input packet processor (28) being capable of producing a destination node (32) based on said destination address; said destination node (32) being forwarded to said routing cache memory (20); a fast packet switch (38); said fast packet switch (38) including a pluraUty of input ports (36); a pluraUty of multi-stage self-routing switch modules (132); a pluraUty of asynchronous packet multiplexers (134); and a pluraUty of output ports (40); said fast packet switch (38) being capable of using said next-node routing tag (30) from said routing cache memory (20) to independently direct a packet (34) processed by said input packet processor (28) through said fast packet switch (38) to one of said plurality of output ports (40) and eventually to one of said plurality of portable (P), mobUe (M) and fixed (F) terminals and gateways (G) and sateUites (S).

Inventors: LIRON MOSHE LERNER, PATTERSON DAVID PALMER, LIRON, MOSHE, LERNER, PATTERSON, DAVID, PALMER
Applicants: CALLING COMMUNICATIONS CORP, CALLING COMMUNICATIONS CORPORATION
Application year: 1992
Main classification: H04L12
IPC codes: H04B7, H04L12, H04Q11