SYSTEM AND METHOD FOR INCREASING FEEDER LINK CAPACITY IN A SATELLITE COMMUNICATIONS SYSTEM

Abstract: A system and method for increasing feeder link capacity in a satellite communication system (100), wherein a gateway (108) communicates with a satellite (102) over a feeder link (112), and wherein the satellite (102) communicates with terrestrial user terminals (106) over a user link (110). A feeder link signal (112) is produced by multiplexing a first BPSK signal and a second BPSK signal (402). The feeder link signal (612) is QPSK modulated, QPSK spread (402). The feeder link signal (612) is transmitted from the gateway (108) to the satellite (102). The satellite (102) demultiplexes the feeder link signal (612), recovering the first and second BPSK signals (702, 704, 706). The first and second BPSK signals are then modulated (502-508)(602-608), to produce a first and second user link signal (832, 834). The user link signals (832, 834) are BPSK modulated, QPSK spread. The user link signals (832, 834) are transmitted from the satellite (102) to the user terminals (106).

Description: SYSTEM AND METHOD FOR INCREASING FEEDER LINK CAPACITY IN A SATELLITE COMMUNICATIONS SYSTEM BACKGROUND OF THE INVENTION I. Field of the Invention The present invention relates generally to satellite communications, and more particularly to increasing feeder link capacity for ground-to-satellite communications by transmitting a QPSK signal formed from two BPSK signals. II. Related Art Today, competing satellite communication systems offer mobile and fixed satellite-based voice and data services that reach the most remote areas of the world at a competitive cost. Users having specially equipped communication devices communicate directly with a satellite orbiting overhead, rather than, for example, with a terrestrial base station as in a conventional cellular network. The satellite (and in some cases, more than one satellite) receives, amplifies, and retransmits these signals to one or more Earth stations, referred to herein as a gateway or hub. The gateway then transfers the information to an existing communications network (for example, a Public Switched Telephone Network (PSTN), a Public Land Mobile Network (PLMN), another gateway) or within the same gateway for transfer to other signal recipients. Similarly, calls originating from an existing communications network pass through the gateway, up to the satellite, and then down to the destination user. Networks of satellites orbiting the earth can provide coverage for vast geographical areas. Satellite communication systems provide economical long distance transmission (cost is not necessarily a function of distance), broad service coverage, freedom from man-made restrictions or natural barriers such as geopolitical boundaries, capability of covering undeveloped areas without having to add a costly land telephone infrastructure, and new service capabilities such as position location. As these satellite communication systems gain users even more users want to make use of such systems and capacity becomes an increasingly important issue. Existing systems employ one or more channelization techniques to increase capacity, such as frequency division multiple access (FDMA), code division multiple access (CDMA), time division multiple access (TDMA), spatial channelization (sometimes called frequency reuse), and polarization multiplexing schemes. A description of satellite communications systems employing code division multiple access (CDMA) spread-spectrum signals, is disclosed in U.S. Patent No. 4,901,307, issued February 13, 1990, entitled "Spread Spectrum Multiple Access Communication System Using Satellite or Terrestrial Repeaters and U. S Patent No. 5,691,974, which issued November 25, 1997, entitled "Method and Apparatus for Using Full Spectrum Transmitted Power in a Spread Spectrum Communication System for Tracking Individual Recipient Phase Time and Energy " both of which are assigned to the assignee of the present invention, and are incorporated herein by reference. On the forward link, information is transmitted from a gateway to a user terminal over one or more beams formed through the use of beam-forming antennas. Each beam covers a particular geographic region within the footprint of the satellite. These beams often comprise a number of so-called subbeams (also referred to as frequency division multiple access (FDMA) channels, or CDMA channels) covering a common geographic area, each occupying a different frequency band. More specifically, in a conventional spread-spectrum communication system, one or more preselected pseudorandom noise (PN) code sequences are used to modulate or "spread" user information signals over a predetermined spectral band prior to modulation onto a carrier signal for transmission as communication signals. In addition, the information signals are typically transferred over both an In-Phase channel using a PNi spreading code and a Quadrature-phase channel using a PN Q code. PN spreading is a method of spread-spectrum transmission that is well known in the art, and produces a communication signal with a bandwidth much greater than that of the data signal. On the forward link, PN spreading codes are generally shared by all communication signals within a given subbeam. In a conventional CDMA spread-spectrum communication system, "channelizing" codes are used to discriminate between different user terminals within a satellite sub-beam on a forward link. The channelizing codes form orthogonal channels in a subbeam over which communication signals are transferred. That is, each user terminal has its own orthogonal channel provided on the forward link by using a unique channelizing orthogonal code. Walsh functions are generally used to implement the channelizing codes, also known as Walsh codes or Walsh sequences, and create what are known as Walsh channels. A typical orthogonal code length is 64 code chips for terrestrial systems and 128 code chips for satellite systems. While the systems discussed above employ channelization techniques to increase capacity, future capacity requirements could demand even more capacity than these conventional techniques can currently provide. For example, the maximum number of users each satellite can service is determined, in part, by the capacity of the gateway-to- satellite communications link, referred to herein as the feeder link. This has been described as the feeder link bandwidth scarcity problem, and occurs regardless of the channelization or modulation technique employed. The bandwidth available to the feeder link must be used in an efficient manner, given that feeder link capacity provides an upper limit to the number of users a particular satellite can service. A need, therefore, exists for an improved system and method for increasing feeder link capacity. SUMMARY OF THE INVENTION Briefly stated, a preferred embodiment of the present invention is directed to a system and method for satellite communications wherein at least one gateway communicates with a satellite over a feeder link, and the satellite communicates with terrestrial user terminals over a user link. A feeder link signal is produced by multiplexing a first binary phase shift keyed (BPSK) signal and a second BPSK signal. The feeder link signal is quadrature phase shift keyed (QPSK) modulated, and QPSK spread. The feeder link signal is transmitted from the gateway to the satellite. The satellite demultiplexes the feeder link signal, recovering the first and second BPSK signals. The first and second BPSK signals are then modulated to produce both first and second user link signals. The two user link signals are then BPSK modulated, and QPSK spread. The user link signals are transmitted from the satellite to one or more user terminals. The current invention increases feeder link capacity by transmitting QPSK modulated, QPSK spread signals over the feeder link rather than BPSK modulated, QPSK spread signals. The feeder link capacity is approximately doubled because both signals have approximately the same bandwidth, but QPSK modulated, QPSK spread signals carry twice the information. This increase in capacity comes at the expense of additional system complexity and hardware costs at the gateway and at the satellite, which is not of great concern in some communication systems that are otherwise capacity limited. An advantage of the current invention is that feeder link capacity can be increased without requiring modifications to existing user equipment that communicates with the satellite using BPSK modulated, QPSK spread signals. This eliminates having to redeploy large numbers of user terminals or wireless equipment to accommodate new users. The QPSK modulated, QPSK spread feeder link signal is demultiplexed at the satellite, forming two BPSK modulated, QPSK spread signals that are then transmitted to the user terminals. Further features and advantages of the invention, as well as the structure and operation of various embodiments of the invention, are described in detail below with reference to the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS The present invention will be described with reference to the accompanying drawings. In the drawings, like reference numbers generally indicate identical, functionally similar, and/or structurally similar elements. The drawing in which an element first appears is indicated by the leftmost digit(s) in the corresponding reference number. FIG. 1 depicts a satellite communications environment within which the present invention is used; FIG. 2A depicts a preferred frequency plan for the forward direction feeder link; FIG. 2B depicts a preferred frequency plan for a user link beam; FIG. 3A depicts a preferred spatial channelization of the forward user link having a footprint divided into beams; FIG. 3B depicts a preferred spatial channelization of the reverse user link having a footprint divided into beams; FIG. 4 depicts a flowchart that describes a preferred method for increasing feeder link capacity; FIG. 5 depicts a flowchart that describes in further detail the production of QPSK/QPSK feeder link signals; FIG. 6 depicts a preferred apparatus for performing the multiplexing operation; FIG. 7 depicts a flowchart that describes demultiplexing the feeder link signal in greater detail; and FIG. 8 depicts a preferred apparatus for performing the demultiplexing operation. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS I. Overview Of The Environment The present invention is directed to a system and method for increasing the feeder link capacity in a satellite communications system. The gateway combines (multiplexes) two BPSK signals to form a QPSK signal. The resulting QPSK signal, referred to herein as a feeder link signal, is then transmitted using the feeder link from the gateway to the satellite. The satellite splits (demultiplexes) the feeder link signal back into two BPSK signals which are transmitted to the user terminals. Feeder link capacity is thereby approximately doubled because the QPSK feeder link signal, which includes the information of two BPSK signals, has approximately the same bandwidth as a single BPSK signal. FIG. 1 depicts a satellite communications environment 100 within which the present invention is useful. A satellite 102, in orbit around Earth 104, communicates with a user terminal 106 over a user link 110. Satellite 102 also communicates with a gateway 108 over a feeder link 112. Satellite 102 is preferably a simple, low cost satellite designed to minimize both production costs and launch costs. Satellite 102 is preferably in a low earth orbit, which permits communication with low power user terminals 106 (for example, wireless devices such as portable phones). However, those skilled in the art will recognize that the principles described herein apply to satellites of varying sophistication and orbit, as well as a variety of wireless devices. User terminal 106 can represent many different communication such as, but not limited to, a wireless telephone, a data transceiver, or a paging or position determination receiver, and can be hand-held, mobile or vehicle mounted, or fixed station units, as desired. A typical hand held unit is similar in design to a conventional cellular phone. In a preferred embodiment, the hand held unit can communicate with terrestrial cellular networks as well as with satellite 102. A typical mobile user terminal includes a hand set and a car kit. The car kit provides battery power, a higher RF power output and a higher gain antenna. Fixed station units communicate with satellite 102, but typically not with other terrestrial cellular networks. The fixed station units are generally used to serve areas that are not served by terrestrial cellular or wireline networks. They are fixed installations with a primary power source, higher RF power and a fixed high gain antenna. Gateway 108 connects user terminal 106 through satellite 102 to other terrestrial communication networks (for example, cellular systems, conventional phone networks, satellite systems) and to other gateways. For example, gateway 108 receives telephone calls or other requests for communication (such as faxes and text messages) from terrestrial switching equipment (not shown) and transmits the calls to the appropriate user terminals 106 using feeder link 112 and user link 110. In the return direction, user terminal 106 transmits to gateway 108 using user link 110 and feeder link 112. Gateway 108 then connects the communication link or call to the terrestrial switching equipment which can then connect to other desired signal recipients through the standard telephone system. Connections can also be made to terrestrial cellular subscribers or to another user terminal 106 directly from the gateway. In a preferred embodiment, gateway 108 employs one or more parabolic antennas 120 to establish feeder link 112. Gateway 108 supports, for example, voice communications, paging, messaging, and data transmissions. Feeder link 112 represents the two-way communication between satellite 102 and gateway 108. In a preferred embodiment, feeder link 112 includes all communications between user terminals 106 serviced by satellite 102 and the terrestrial communication networks connected to gateway 108. Feeder link 112 also includes other communications, such as telemetry and control commands transferred between gateway 108 and satellite 102 or user terminals 106. FIG. 2A depicts a preferred frequency plan for the forward direction feeder link 112 (that is, from gateway 108 to satellite 102). Communications between gateway 108 and satellite 102 employ FDMA, CDMA, and polarization multiplexing schemes to make efficient use of the available bandwidth. As shown in FIG. 2A, the frequency band of feeder link 112 is divided into two or more channels 202, corresponding to user links 110. In a preferred embodiment, the band is divided into eight channels 202 (I, K, M, O, H, C, G, and D) employing right hand circular polarization (RHCP) and eight channels 202 (L, N, P, J, A, F, E, and B) employing left hand circular polarization (LHCP). In a typical system design, each channel 202 preferably covers a 16.5 MHz wide bandwidth, spaced 19.38 MHz apart between 5091 MHz and 5250 MHz. Feeder link 112 also includes a command channel 204 that carries command information between satellite 102 and gateway 108. FIG. 2B depicts a preferred frequency plan for an example channel 202. As shown, each channel 202 is made up of two or more (preferably 13) FDMA subchannels 204, also referred to as user link beams or CDMA channels in a CDMA communication system. Each user link beam 204 is further divided into two or more orthogonal code channels typically implemented using Walsh code sequences (preferably up to 128). For example, a user link beam 204 might contain 128 signals or signal channels, each destined for a different user terminal 106, where each signal is BPSK modulated according to conventional techniques. Many different types of information can be transmitted over each CDMA channel including, but not limited to, voice and data. A similar frequency plan is preferably employed for the reverse direction feeder link 112, with the channels 202 spaced between 6875 MHz and 7075 MHz. Otherwise, the reverse direction feeder link 112 is substantially identical to the forward link described with respect to FIG. 2 A and 2B. User link 110 represents the two-way communication between satellite 102 and user terminals 106 serviced by satellite 102. In a preferred embodiment, user link 110 employs spatial channelization to make efficient use of the available spectrum. Spatial channelization can be employed to divide the terrestrial area serviced by a satellite, referred to herein as the satellite's footprint, into two or more service regions. Spatial channelization is made possible by various techniques for producing beams, that is, the directional transmission of electromagnetic energy. A beam is formed for each region, such that most of the energy transmitted using a beam illuminates the ground within the service region. This allows a small set of frequencies to be reused in known patterns across the footprint. CDMA communications systems allow the same set of frequencies to be used in adjacent regions. It is understood that similar techniques are used for receiving signals that are transmitted by users within the service region at the satellite. Again, the general concepts described herein apply to other embodiments employing alternative techniques for increasing capacity. FIG. 3A depicts the spatial channelization of user link 110 divided into beams 302A through 302P, referred to collectively as an antenna beam configuration 300A. The outer perimeter of antenna beam configuration 300A defines the approximate limits of the geographic region serviced by satellite 102. Those user terminals 106 within this region are serviced by (at least) satellite 102. Antenna beam configuration 300A is preferably used in the forward direction (that is, from satellite 102 to user terminals 106) user link 110. In one alternative embodiment, each beam transmits signals with substantially uniform strength across the area defined for it in FIG. 3A, including an appropriate compensation for the curvature of the earth (that is, an isoflux pattern). However, each pattern preferably takes into account any non-uniform distribution of user terminals 106 across each beam 302, as described in commonly owned, co-pending U.S. Patent Application Serial No. 09/378,562, filed August 19, 1999, entitled "Satellite Communication System Using Wide Fixed Beams And Narrow Steerable Beams, " which is incorporated herein by reference. FIG. 3B depicts an alternative antenna beam configuration 300B, which is preferably used in the reverse direction of user link 110 (that is, from user terminals 106 to satellite 102). Comparing FIGS. 3 A and 3B illustrates that the antenna beam configurations for the forward and reverse user links are preferably different from one another. Other alternative embodiments use the same antenna beam configurations for both. Satellite 102 essentially acts as a transponder, receiving signals from a gateway, hub, fixed or base-station 108 over feeder link 112 and re-transmitting them to user terminals 106 over user link 110. Satellite 102 demultiplexes the signals on feeder link 112 into two or more channels 202 and command channel 204, where used. All communications destined for those user terminals 106 within a given beam 302 are transmitted over a single channel 202. The individual user terminals 106 then select their assigned code channel within a subbeam or CDMA channel according to spread spectrum techniques known to those skilled in the art. Though not discussed herein, satellite 102 also acts as a transponder to route reverse user link 110 to gateway 108 using reverse feeder link 112. A network of satellites 102 is preferably deployed having partially overlapping service areas. This network can provide service to user terminals 106 over large geographic areas, as is well known. In a preferred embodiment, the subchannel signal or user link beam transmitted over user link 110 takes the form: X*PNι *cos(ω c t) + X*PN Q *)sin(ui-t) where X is the sum of the binary data modulated Walsh codes for those user terminals 106 assigned to the particular user link beam 204, PNj is an in-phase pseudo- noise (PN) spreading sequence, PN Q is a quadrature phase PΝ spreading sequence, and ύ) c is the center frequency of user link beam 204 over which the signal is being transmitted. These signals are described as BPSK modulated, QPSK spread (BPSK/QPSK): BPSK modulated because X represents the same information signal, X, which modulates both the in-phase and quadrature components; and QPSK spread because the signal employs two different spreading sequences (PN / and PN Q ). This differs from true QPSK modulation in that only one signal (X) is driving both the in- phase and quadrature components. User terminals 106 receive this user link beam signal, despread the in-phase and quadrature portions using the spreading sequences, and then select their assigned code channel. This BPSK/QPSK signal is preferably transmitted over user link 110. As mentioned above, in newer or next generation satellite communication systems it will be desirable to add additional user capacity. This may require the addition of more beams on the user link, and associated subchannels on the feeder link. However, in order to accommodate existing systems, regulatory frequency allocations, and so forth, there is a need or desire to stay within the same allocated feeder bandwidth. Therefore, a technique is needed that allows additional beams to be transferred over the feeder link within that existing bandwidth. Even when additional bandwidth is available, there may still exist certain constraints that unacceptably limit the number of beams possible using current approaches. As described below, according to the present invention, the BPSK/QPSK signal is replaced with a QPSK modulated / QPSK spread signal (QPSK/QPSK) signal for transmission over feeder link 112. As a result, twice as many user link signals can be transmitted over feeder link 112 without increasing the required bandwidth. Feeder link 112 capacity is, therefore, doubled. II. Overview Of The Invention FIG. 4 depicts a flowchart that describes a preferred method according to the present invention for increasing the capacity of feeder link 112. In step 402, two BPSK signals are multiplexed together to produce a QPSK/QPSK feeder link signal. This multiplexing operation is preferably performed by gateway 108, although it can be implemented elsewhere as desired. In step 404, the QPSK/QPSK feeder link signal is transmitted via feeder link 112 from gateway 108 to satellite 102. In step 406, satellite 102 demultiplexes the QPSK/QPSK signal back into the two original BPSK signals. In step 408, the two BPSK signals are modulated to form BPSK/QPSK user link signals. In step 410, the user link signals are transmitted via user link 110 from satellite 102 to user terminals 106. Transmitting QPSK/QPSK feeder link signals rather than BPSK/QPSK effectively doubles the feeder link capacity, because both require approximately the same bandwidth but QPSK/QPSK carries twice the information. For current communication system designs, this increase in capacity would come at the expense of additional hardware being added to satellite 102 to demultiplex and re-modulate the QPSK/QPSK feeder link signals. The following sections describe these steps in detail. III. Producing QPSK QPSK Feeder Link Signals FIG. 5 depicts a flowchart that describes in further detail the production of QPSK/QPSK feeder link signals in step 402. These operations are described in conjunction with FIG. 6, which depicts a preferred apparatus, multiplexer 600, for performing the multiplexing operation. Multiplexer 600 includes eight modulators 602A, 602B, 602C, 602D, 604A, 604B, 604C, and 604D, and two adders 608A and 608B. However, the function of adders 608A and 608B could be performed by a single logical adder element, although usually less convenient to implement. Multiplexer 600 accepts two BPSK signal inputs, shown as X and Y in FIG. 6, and outputs a QPSK/QPSK feeder link signal 612. Multiplexer 600 is preferably located in gateway 108. but those skilled in the art will recognize that these operations could equivalently be performed elsewhere so long as a communications pathway is established with gateway 108. In step 502, the first BPSK signal, X as shown in FIG. 6, is modulated by an in- phase PN spreading code {PNf) and a carrier signal to produce a first signal component 606A. Modulator 602A modulates X by PN], generally by multiplication, and modulator 604A modulates the output of modulator 602A by cos(coιt). The resulting first signal component can be expressed as X*PNι*cos(Cύ t t). In step 504, X is modulated by a quadrature phase PN spreading code {PN Q ) and a quadrature phase carrier signal to produce a second signal component 606B. Modulator 602B modulates X by PN Q and modulator 604B modulates the output of modulator 602B by sin(ω c t). The resulting second signal component can be expressed as X*PNo*sin(θ)tt). In step 506, the second BPSK signal, Y as shown in FIG. 6, is modulated by PN / and the quadrature phase carrier signal to produce a third signal component 606C. Modulator 602C modulates Y by PNj while modulator 604C modulates the output of modulator 602C by sin(o^t). The resulting third signal component can be expressed as Y*PN I *sin(ω b t)- In step 508, Y is modulated by PN Q and the carrier signal to produce a fourth signal component. Modulator 602D modulates Y by PN Q . while modulator 604D modulates the output of modulator 602D by cos(cott). The resulting fourth signal component can be expressed as Y*PN Q *cos(ύJt;t). Next, the process adds or sums the first, second, and third, signal components (606 A, 606B, and 606C) together while subtracting, or performing a sign reversed summation of, the fourth signal component (606D). This can be thought of as using a single summation element in a step 509, with is a functional combination of elements 608A and 608B shown in FIG. 6, to perform this summation. However, in a preferred embodiment, the summation processing is subdivided into smaller steps using the individual summation elements 608A and 608B shown in FIG. 6. It will be readily apparent to those skilled in the art that this is presented as an example implementation technique and that fewer more complex or more less complex elements may be used to implement the desired summation or combination of signals. In step 510, the second, and third signal components 606B and 606C are summed to produce a fifth signal component. Adder 608A performs this summing operation. In step 512, the difference between the sum of the first (606A) and fifth signal components and the fourth signal component (606D) is calculated, with the result being feeder link signal 606. As shown in FIG. 6, adder 608B performs this difference operation as a summation of the first (606A), fourth (606D), and fifth signal components, with the fourth signal component having a negative input. Again, those skilled in the art will readily appreciate that other groupings of two or three signals and more or fewer summation or combinatorial logic elements, or other orders or arrangements of the signals for summation, can be employed to reach the desired summation or combination of signals without departing from the teachings of the present invention. The resulting feeder link signal 612 can be expressed as: {X*PNj - Y*PN Q )cos(ω c t) + {X*PN Q + Y*PNι)sin(tø) where X*PN / - Y*PN Q is referred to as the in-phase component of feeder link signal 612, and X*PNQ + Y*PNι is referred to as the quadrature phase component of feeder link signal 612. In a preferred embodiment, X represents the sum of binary data modulated orthogonal, Walsh, codes for those user terminals 106 assigned to a single user link beam 204. However, in other alternative embodiments X can represent any arbitrary signal input. For example, X can represent a single signal, or the combination of two or more signals. Furthermore, X is not limited to digital modulation, and may represent analog modulated or unmodulated signals. Skilled artisans will recognize that multiplexer 600 can be implemented as hardware, software, or a combination of both. For instance, a modulator 602 or 604 (602A, 602B, 602C, 602D, 604A, 604B, 604C, 604D) can represent a hardware multiplier, or equivalently, a software routine for multiplying two signals. Similarly, an adder 608 (608A, 608B) can represent a hardware adder, or equivalently, a software routine for adding two or more signals. Those skilled in the art will also recognize that many variations of multiplexer 600 are possible, having different combinations of modulators, adder, or other functional units, combined to produce feeder link signal 612. The components of multiplexer 600 as shown in FIG. 6 were chosen primarily for ease of explanation. IV. Demultiplexing Feeder Link Signals Returning to FIG. 4, in step 404, feeder link signal 612 is transmitted from gateway 108 to satellite 102 according to conventional satellite communication techniques. Feeder link signal 612 is preferably transmitted over a particular user link beam 204 of feeder link 112, as described above. In step 406, feeder link signal 612 is demultiplexed at satellite 102, producing the two BPSK signals that were combined to form feeder link signal 612 at gateway 108 {X and Y as shown in FIG. 6). FIG. 7 depicts a flowchart that describes step 406 in greater detail. These operations are described in conjunction with FIG. 8, which depicts a preferred apparatus for performing the demultiplexing operation, transponder 800. Transponder 800 includes a demultiplexer 802 and a user link modulator 804, and is preferably located in satellite 102. In step 702, feeder link signal 612 is demodulated into in-phase and quadrature components. As shown in FIG. 8, demultiplexer 802 includes six demodulators 812 A, 812B, 814A, 814B, 814C, and 814D, two adders 816A and 816B, a voltage controlled oscillator (VCO) 806, and a 90° phase shifter 808. Demultiplexer 802 receives feeder link signal 612 from a receiving antenna on satellite 102 (not shown), which is fed into demodulators 812A and 812B. Skilled artisans will recognize that oftentimes additional modulation stages are required between the antenna and transponder 800, such as to convert signals from one RF frequency to another in line with allocated link frequencies, or to down-convert from RF to IF frequencies. These additional stages are not depicted or discussed further herein, as their design and implementation are well within the conventional art. VCO 806 generates the carrier signal cos(cθtt) that is in phase with the carrier signal used in feeder link signal 612. Demultiplexer 802, therefore, preferably performs coherent demodulation. Conventional techniques are employed to ensure that coherency is maintained. The output of phase shifter 808 is the quadrature phase carrier signal sin(ω c t). Demodulator 812A demodulates feeder link signal 612 by the carrier signal, producing the in-phase component of feeder link signal 612, X*PNj - Y*PN Q . Demodulator 812B demodulates feeder link signal 612 by the quadrature phase carrier signal, producing the quadrature phase component of feeder link signal 612, X*PN Q + Y*PN, . In step 704, the first BPSK signal X is extracted by adding the in-phase component multiplied by PN/ to the quadrature phase component multiplied by PN Q . Demodulator 814A multiplies the in-phase component by PN, producing X*PN 2 - Y*PN / PN Q . Demodulator 814B multiplies the quadrature phase component by PN Q , producing X*PN Q 2 + Y*PN / PN Q . Note that the spreading codes PN / and PN Q must be known by satellite 102 and synchronized with the codes in feeder link signal 606. Adder 816A sums the output of demodulator 814A with the output of demodulator 814B, producing 2*X,{ recognizing that PN = PN Q 2 = 1). In step 706, the second BPSK signal Y is extracted by obtaining the difference between the in-phase component multiplied by PN Q and the quadrature phase component multiplied by PN / . Demodulator 814C multiplies the in-phase component by PN Q , producing X*PN / PN Q - Y*PN Q 2 . Demodulator 814D multiplies the quadrature phase component by PN producing X*PNιPN β + Y*PN?. Adder 816B sums the output of demodulator 814C with the negative or sign reversed output of demodulator 814D, producing 2*Y. Demultiplexer 802, therefore, has two outputs, 2*X and 2*7. V. User Link Modulation Returning again to FIG. 4, in step 408, the two BPSK signals are modulated to produce two BPSK modulated, QPSK spread user link signals. As shown in FIG. 8, user link modulator 804 includes eight demodulators 822A, 822B, 822C, 822D, 824A, 824B, 824C, 824D, two adders 826A, 826B, a VCO 818, and a 90° phase shifter 820. The first BPSK/QPSK signal 832 is produced by the operation of demodulators 822A, 822B, 824A, and 824B, and adder 826A. Demodulator 822A demodulates the output of adder 816A, 2*X, by PN Q , the output of which is then multiplied by sin(oi t) in demodulator 824A, producing 2*X*PN Q sin(ct)tt). The frequency ύϋt is the center frequency of the appropriate user link beam 204, as transmitted within a given beam 302 over user link 110 (as described above). Demodulator 822B demodulates the output of adder 816A by PN, the output of which is then multiplied by cos(ύχt) in demodulator 824B, producing 2*X*PNιcos(ωtt). Adder 826A sums the output of demodulator 824A with the output of demodulator 824B, producing a first BPSK/QPSK user link signal 832, given by: 2*X*PN,cos(ω c t) + 2*X*PN Q sin( ) Note that user link signal 832 has the proper form for transmission over user link 110, as described above. The second BPSK/QPSK signal 834 is produced by the operation of demodulators 822C, 822D, 824C, and 824D, and adder 826B. Demodulator 822A demodulates the output of adder 816B, 2*Y, by PN Q , the output of which is then multiplied by cos(ω c t) in demodulator 824C, producing 2*Y*PN Q Cos(cθ c t). Demodulator 822D demodulates the output of adder 816B by PN, the output of which is then multiplied by sinfa^t) in modulator 824D, producing 2*Y*PNιsin(cϋit). Adder 826B sums the output of demodulator 824D with the output of demodulator 824C, producing a second BPSK/QPSK user link signal 834, given by: 2*Y*PN Q cos(ω c t) + 2*Y*PN,sin(ύ)kt) Note that user link signal 814 has the proper form for transmission over user link 110, as described above. Returning to FIG. 4, in step 410 user link signals 832 and 834 are transmitted via user link 110 to user terminals 106. This transmission is accomplished according to the above description and conventional satellite-to-ground communication techniques. VI. Conclusion The previous description of the preferred embodiments is provided to enable any person skilled in the art to make or use the present invention. While the invention has been particularly shown and described with reference to preferred embodiments thereof, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention. What I claim as my invention is:

Claims: CLAIMS 1. A method for satellite communications wherein a gateway communicates with a satellite over a feeder link, and wherein the satellite communicates with terrestrial user terminals over a user link, comprising the steps of: multiplexing a first BPSK signal and a second BPSK signal to produce a feeder link signal, wherein said feeder link signal is QPSK modulated, QPSK spread; transmitting said feeder link signal from the gateway to the satellite; demultiplexing said feeder link signal to produce said first and second BPSK signals; modulating said first BPSK signal to produce a first user link signal, wherein said first user link signal is BPSK modulated, QPSK spread; modulating said second BPSK signal to produce a second user link signal, wherein said second user link signal is BPSK modulated, QPSK spread; and transmitting said first and second user link signals from the satellite to the user terminals. 2. The method of claim 1, wherein said step of multiplexing a first BPSK signal and a second BPSK signal comprises the steps of: modulating said first BPSK signal with an in-phase PN code and a carrier signal to produce a first signal component; modulating said first BPSK signal with a quadrature -phase PN code and a quadrature phase of said carrier signal to produce a second signal component; modulating said second BPSK signal with said in-phase PN code and said quadrature phase of said carrier signal to produce a third signal component; modulating said second BPSK signal with said quadrature-phase PN code and said carrier signal to produce a fourth signal component; summing said first, second, and third signal components to the negative of said fourth signal component to produce a feeder link signal. 3. The method of claim 2, wherein said step of summing comprises the steps of: summing said second, and third signal components to produce a fifth signal component; and summing said first and fifth signal components to the negative of said fourth signal component to produce said feeder link signal. 4. The method of claim 2, wherein said step of demultiplexing said feeder link signal comprises the steps of: demodulating said feeder link signal into an in-phase component and a quadrature component; adding said in-phase component multiplied by said in-phase PN code to said quadrature phase component multiplied by said quadrature phase PN code to extract said first BPSK signal; and obtaining the difference between said in-phase component multiplied by said quadrature phase PN code and said quadrature phase component multiplied by said in- phase PN code to extract said second BPSK signal. 5. The method of claim 1, wherein said first BPSK signal comprises a first sum of binary data modulated Walsh codes, and wherein said second BPSK signal comprises a second sum of binary data modulated Walsh codes. 6. A method for increasing the capacity of a feeder link in a satellite communications system, comprising the steps of: modulating a first signal with an in-phase PN code and a carrier signal to produce a first signal component; modulating said first signal with a quadrature-phase PN code and a quadrature phase of said carrier signal to produce a second signal component; modulating a second signal with said in-phase PN code and said quadrature phase of said carrier signal to produce a third signal component; modulating said second signal with said quadrature-phase PN code and said carrier signal to produce a fourth signal component; summing said first, second, and third signal components to the negative of said fourth signal component to produce a feeder link signal. 7. The method of claim 6, wherein said step of summing comprises the steps of: summing said second, and third signal components to produce a fifth signal component; and summing said first and fifth signal components to the negative of said fourth signal component to produce said feeder link signal. 8. A satellite communications system wherein a gateway communicates with a satellite over a feeder link, and wherein the satellite communicates with terrestrial user terminals over a user link, comprising: means for multiplexing a first BPSK signal and a second BPSK signal to produce a feeder link signal, wherein said feeder link signal is QPSK modulated, QPSK spread; means for transmitting said feeder link signal from the gateway to the satellite; means for demultiplexing said feeder link signal to produce said first and second BPSK signals; means for modulating said first BPSK signal to produce a first user link signal, wherein said first user link signal is BPSK modulated, QPSK spread; means for modulating said second BPSK signal to produce a second user link signal, wherein said second user link signal is BPSK modulated, QPSK spread; and means for transmitting said first and second user link signal from the satellite to the user terminals. 9. The system of claim 8, wherein said means for multiplexing comprises: means for modulating said first BPSK signal with an in-phase PN code and a carrier signal to produce a first signal component; means for modulating said first BPSK signal with a quadrature-phase PN code and a quadrature phase of said carrier signal to produce a second signal component; means for modulating said second BPSK signal with said in-phase PN code and said quadrature phase of said carrier signal to produce a third signal component; means for modulating said second BPSK signal with said quadrature-phase PN code and said carrier signal to produce a fourth signal component; means for summing said first, second, and third signal components to the negative of said fourth signal component to produce said feeder link signal. 10. The system of claim 9, wherein said means for demultiplexing comprises: means for demodulating said feeder link signal into an in-phase component and a quadrature component; means for adding said in-phase component multiplied by said in-phase PN code to said quadrature phase component multiplied by said quadrature phase PN code to extract said first BPSK signal; and means for obtaining the difference between said in-phase component multiplied by said quadrature phase PN code and said quadrature phase component multiplied by said in-phase PN code to extract said second BPSK signal. 11. The system of claim 8, wherein said first BPSK signal comprises a sum of binary data modulated Walsh codes, and wherein said second BPSK signal comprises a sum of binary data modulated Walsh codes. 12. A multiplexer for increasing the capacity of a feeder link in a satellite communications system, comprising: means for modulating a first signal with an in-phase PN code and a carrier signal to produce a first signal component; means for modulating said first signal with a quadrature-phase PN code and a quadrature phase of said carrier signal to produce a second signal component; means for modulating a second signal with said in-phase PN code and said quadrature phase of said carrier signal to produce a third signal component; means for modulating said second signal with said quadrature-phase PN code and said carrier signal to produce a fourth signal component; means for summing said first, second, and third signal components to the negative of said fourth signal component to produce a feeder link signal. 13. The multiplexer of claim 12 wherein said means for summing comprises: means for summing said second, and third signal components to produce a fifth signal component; and means for summing said first and fifth signal components to the negative of said fourth signal component to produce said feeder link signal.

Inventors: SCHIFF LEONARD N, SCHIFF, LEONARD, N.
Applicants: QUALCOMM INC, QUALCOMM INCORPORATED
Application year: 2000
Main classification: H04B7
IPC codes: H04B7, H04L5