# Patent

## Title
Pilot pattern for observation scalar MIMO-OFDM

## Abstract

In an embodiment, a transmitter includes first and second transmission paths. The first transmission path is configurable to generate first pilot clusters each including a respective first pilot subsymbol in a first cluster position, and the second transmission path is configurable to generate second pilot clusters each including a respective second pilot subsymbol in a second cluster position such that a vector formed by the first pilot subsymbols is orthogonal to a vector formed by the second pilot subsymbols. For example, where such a transmitter transmits simultaneous orthogonal-frequency-division-multiplexed (OFDM) signals (e.g., MIMO-OFDM signals) over respective channels that may impart inter-carrier interference (ICI) to the signals due to Doppler spread, the pattern of the pilot symbols that compose the pilot clusters may allow a receiver of these signals to use a recursive algorithm, such as a Vector State Scalar Observation (VSSO) Kalman algorithm, to estimate the responses of these channels.

## Background
PRIORITY CLAIM
The present application claims the benefit of priority to the following applications, and is a Continuation-in-Part of copending U.S. patent application Ser. No. 12/963,569, filed Dec. 8, 2010, which application claims the benefit of U.S. Provisional Patent Application Nos. 61/267,667, filed Dec. 8, 2009, and 61/360,367, filed Jun. 30, 2010, and which application is a Continuation-in-Part of copending U.S. patent application Ser. No. 12/579,935, filed Oct. 15, 2009, and Ser. No. 12/579,969, filed Oct. 15, 2009, which applications claim the benefit of U.S. Provisional Patent Application Ser. Nos. 61/105,704, filed Oct. 15, 2008, and 61/158,290, filed Mar. 6, 2009; the present application also claims the benefit of U.S. Provisional Patent Application Ser. No. 61/495,218, filed Jun. 9, 2011; all of the foregoing applications are incorporated herein by reference in their entireties.
RELATED APPLICATION DATA
The present application is related to copending U.S. patent application Ser. No. 13/284,879, entitled “DETERMINING RESPONSES OF RAPIDLY VARYING MIMO-OFDM COMMUNICATION CHANNELS USING OBSERVATION SCALARS”, filed Oct. 29, 2011; U.S. patent application Ser. No. 13/284,894, entitled “DETERMINING A RESPONSE OF A RAPIDLY VARYING OFDM COMMUNICATION CHANNEL USING AN OBSERVATION SCALAR”, filed Oct. 29, 2011; and U.S. patent application Ser. No. 13/284,898, entitled “PILOT PATTERN FOR MIMO-OFDM”, filed Oct. 29, 2011; all of the foregoing applications are incorporated herein by reference in their entireties.


SUMMARY
In an embodiment, a transmitter includes first and second transmission paths. The first transmission path is configurable to generate first pilot clusters each including a respective first pilot subsymbol in a first cluster position, and the second transmission path is configurable to generate second pilot clusters each including a respective second pilot subsymbol in a second cluster position such that a vector formed by the first pilot subsymbols is orthogonal to a vector formed by the second pilot subsymbols.
For example, where such a transmitter transmits simultaneous orthogonal-frequency-division-multiplexed (OFDM) signals (e.g., MIMO-OFDM signals) over respective channels that may impart inter-carrier interference (ICI) to the signals due to Doppler spread, the pattern of the pilot symbols that compose the pilot clusters may allow a receiver of these signals to use a recursive algorithm, such as a Vector State Scalar Observation (VSSO) Kalman algorithm, to estimate the responses of these channels. Such a receiver may estimate the channel responses more accurately, more efficiently, with a less-complex algorithm (e.g., with an algorithm that does not require a real-time matrix inversion), and with less-complex software or circuitry, than conventional receivers.



BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a block diagram of an embodiment of base and client orthogonal-frequency-division-multiplexing (OFDM) transmitter-receivers that are not moving significantly relative to one another while they are communicating with one another.
FIG. 2 is a plot of an embodiment of the frequencies of the carrier signals (solid lines) generated by the presently transmitting transmitter-receiver of FIG. 1, and of the frequency “slots” (dashed lines) that these carrier signals may respectively occupy at the presently receiving transmitter-receiver of FIG. 1.
FIG. 3 is a block diagram of an embodiment of base and client OFDM transmitter-receivers that are moving relative to one another while they are communicating with one another.
FIG. 4 is a plot of an embodiment of the frequencies of carrier signals (solid lines) generated by the presently transmitting transmitter-receiver of FIG. 3, and of the frequency slot (dashed line) that the center one of these plotted carrier signals may occupy at the presently receiving transmitter-receiver of FIG. 3.
FIG. 5 is a plot of an embodiment of the frequencies of carrier signals generated by the presently transmitting transmitter-receiver of FIG. 3, where the carrier signals are grouped into clusters of data carrier signals (data clusters) and clusters of pilot carrier signals (pilot clusters).
FIG. 6 is a plot of an embodiment of data clusters and pilot clusters generated by the presently transmitting transmitter-receiver of FIG. 3, where the pilot clusters have a uniform separation.
FIG. 7 is a plot of an embodiment of a pilot cluster.
FIG. 8 is a plot of another embodiment of a pilot cluster.
FIG. 9 is a block diagram of an embodiment of the receiver of one or both of the base and client transmitter-receivers of FIG. 3.
FIG. 10 is a block diagram of an embodiment of the channel estimator of FIG. 9.
FIG. 11 is a diagram of an embodiment of base and client MIMO-OFDM transmitter-receivers that are moving relative to one another while they are communicating with one another, and of the communication paths between multiple base transmit antennas and a single client receive antenna.
FIG. 12 is a diagram of an embodiment of base and client MIMO-OFDM transmitter-receivers that are moving relative to one another while they are communicating with one another, and of the communication paths between multiple base transmit antennas and multiple client receive antennas.
FIG. 13 is a block diagram of an embodiment of the receiver of one or both of the base and client transmitter-receivers of FIGS. 11 and 12.
FIG. 14 is a block diagram of an embodiment of a portion of the channel estimator of FIG. 13, the portion associated with a single receive antenna.
FIG. 15 is a block diagram of an embodiment of a partial-channel-estimation-matrix combiner of the channel estimator of FIG. 13.
FIG. 16 is a block diagram of an embodiment of the received-signal combiner of FIG. 13.
FIG. 17 is a block diagram of an embodiment of a transmitter of one or both of the base and client transmitter-receivers of FIGS. 11 and 12.



DETAILED DESCRIPTION
FIG. 1 is a block diagram of an embodiment of a base transmitter-receiver 10 and of a client transmitter-receiver 12, which communicates with the base transmitter-receiver over a wireless channel 14 via multicarrier signals (e.g., OFDM signals) while remaining substantially stationary relative to the base transmitter-receiver. For example, the base 10 may be a wireless router in a home or office, and the client 12 may be a computer that communicates with the base via OFDM signals that have N carriers. One or more antennas 16 are coupled to the base 10, and one or more antennas 18 are coupled to the client 12. Each antenna 16 may function as only a transmit antenna, as only a receive antenna, or as a transmit-receive antenna; and each antenna 18 may function similarly. Furthermore, the channel 14 may include Z multiple paths L0-Lz-1 over which the multicarrier signals propagate. For example, a first path L0 may be a straight-line path between the antennas 16 and 18, and a second path L1 may be a multi-segmented path that is caused by signal reflections from one or more objects (not shown in FIG. 1) near the base 10, client 12, or channel 14.
FIG. 2 is a frequency plot of some of the N carriers (here, carriers N−a to N−(a−8) are shown in solid line and are hereinafter called “subcarriers”) of an embodiment of an OFDM data symbol 20, which may be transmitted by the base 10 of FIG. 1 and received by the client 12, or vice versa—an OFDM data symbol is a portion of an OFDM signal that is modulated with the same data subsymbols for a symbol period. Each of the subcarriers N−a to N−(a−8) has a respective frequency fN-a-fN-(a-8), and is orthogonal to the other subcarriers. In this context, “orthogonal” means that, in the absence of inter-carrier interference (discussed below) and noise, one may construct a time-domain signal from these modulated subcarriers (e.g., using an Inverse Fast Fourier Transform (IFFT)), and then extract these modulated subcarriers, and the information that they carry, from the time-domain signal (e.g., using a Fast Fourier Transform (FFT)) with no loss of information. Furthermore, although the base 10 is described as transmitting the OFDM signal in the example below, it is understood that this example would be similar if the client 12 were transmitting the OFDM signal.
Referring to FIGS. 1 and 2, the transmitter of the base 10 modulates each of at least some of the N subcarriers with a respective data value (hereinafter a data subsymbol) for a time period hereinafter called a symbol period—the transmitter may not use one or more of the N subcarriers due to, for example, excessive interference at the frequencies of these subcarriers. Examples of suitable modulation schemes include binary phase-shift keying (BPSK), quadrature phase-shift keying (QPSK), and quadrature amplitude modulation (QAM), the latter two schemes providing data subsymbols that each have multiple bits.
The frequency spacing fs between adjacent ones of the N subcarriers is typically constant, and is conventionally selected to minimize inter-carrier interference (ICI), which is a phenomenon that occurs if energy from one subcarrier “spills over” to the frequency slot of another subcarrier at the receiver of the client 12. At the transmitter of the base 10, each of the active ones of the N subcarriers has a frequency fk (for k=0 to N−1) represented by a respective one of the solid lines (only the frequencies fk for k=N−a to N−(a−8) are shown in FIG. 2). But at the receiver of the client 12, the respective frequency fk of each subcarrier may be effectively shifted within a respective frequency slot 22 indicated by the dashed lines (only the slots 22 of the frequencies fk for k=N−a to N−(a−8) are shown in FIG. 2). For example, at the receiver of the client 12, the frequency fN-a, of the subcarrier N−a may be shifted to another location within the frequency slot 22N-a, or may be “spread” over multiple locations within this frequency slot. Causes for this frequency shifting/spreading may include, for example, the existence of multiple transmission paths L (i.e., Z>1), and channel conditions (e.g., humidity, temperature) that may effectively shift the respective phase and attenuate the respective amplitude of each modulated subcarrier.
To allow the receiver of the client 12 to recover the data subsymbols in the presence of ICI and other interference or noise, the transmitter of the base 10 transmits an OFDM training symbol—a “training symbol” is the combination of all the training subsymbols transmitted during a training-symbol period—shortly before transmitting an OFDM data symbol—a “data symbol” is the combination of all of the data subsymbols transmitted during an OFDM data-symbol period. That is, the transmitter of the base 10 transmits the training symbol during a first OFDM symbol period, and transmits the data symbol during a second, subsequent OFDM symbol period. Because the receiver of the client 12 “knows” the identity of the transmitted training symbol ahead of time, the receiver characterizes the channel 14 by comparing the received training symbol with the known transmitted training symbol. For example, the receiver may characterize the channel 14 by generating an N×N matrix Ĥ of estimated complex frequency-domain coefficients that respectively represent the estimated frequency response (e.g., the imparted ICI, amplitude attenuation, and phase shift) of the channel at each of the subcarrier frequencies fk—the “^” indicates that Ĥ is an estimate of the actual channel matrix H. As discussed in more detail below, the receiver may then use this channel-estimation matrix Ĥ to recover transmitted data symbols from respective received data symbols.
FIG. 3 is a block diagram of an embodiment of the base transmitter-receiver 10 and of the client transmitter-receiver 12 of FIG. 1, but where the base and client are moving relative to one another at a non-zero velocity (the velocity may be constant or time varying) while they are communicating with one another, and where like numbers refer to components common to FIGS. 1 and 3. For example, the base 10 may be a cell tower, and the client 12 may be an internet-capable phone that is located within a moving automobile 24. The base 10 and the client 12 may communicate with one another according to one or more communications standards that specify OFDM technology for mobile communications. These standards include, for example, the DVB-H standard and the WiMAX standard. Furthermore, although only the client 12 is shown as moving, in other embodiments the base 10 may be moving and the client 12 may be stationary, or both the base and the client may be moving simultaneously.
FIG. 4 is a frequency plot of some of the N subcarriers (here, subcarriers N−a to N−(a−8) in solid line) of an embodiment of an OFDM symbol 25 that may be transmitted by the base 10 of FIG. 1 and received by the client 12, or vice versa. Although the base 10 is described as transmitting the OFDM symbol in the example below, it is understood that this example would be similar if the client 12 were transmitting the OFDM symbol.
At the base 10, the OFDM symbol may be similar to the OFDM symbol of FIG. 2 in that the base modulates each of at least some of the N subcarriers with a respective data subsymbol, and each of the data-modulated ones of the N subcarriers has a center frequency fk represented by a respective one of the solid lines.
But at the receiving client 12, the frequency fk of a subcarrier k may be shifted/spread by one or more times fs as indicated by the frequency slot 26N-(a-4) of the subcarrier k=N−(a−4) (only this one frequency slot is shown in FIG. 3 for clarity) such that energy from a subcarrier k may spill over to the frequencies of one or more adjacent subcarriers (e.g., k−1, k+1) on either side of the subcarrier k. For example, in the embodiment shown in FIG. 4, energy from the subcarrier k=N−(a−4) may spill over to the frequencies fN-a-fN-(a-3) and fN-(a-5)-fN-(a-8) of the subcarriers k=N−a to N−(a−3) and k=N−(a−5) to N−(a−8).
The frequency shifts/spreads of the received OFDM subcarriers of FIG. 4 may be significantly greater than the frequency shifts/spreads of the received OFDM subcarriers of FIG. 2 because, in addition to the causes for this frequency shifting/spreading described above (e.g., the existence of multiple transmission paths L and channel conditions), the received OFDM subcarriers of FIG. 4 may also experience respective Doppler shifts caused by the relative movement between the base 10 and the client 12.
According to the Doppler Effect, the frequency of a signal at a receiver is different from the frequency of the signal at a transmitter if the receiver and transmitter are moving relative to one another at a non-zero velocity. If the receiver and transmitter are moving away from one another, then the frequency of the signal at the receiver is typically lower than the frequency of the signal at the transmitter; conversely, if the receiver and transmitter are moving toward one another, then the frequency of the signal at the receiver is typically higher than the frequency of the signal at the transmitter. For example, a person (receiver) who is listening to the whistle of an approaching train (transmitter) may experience this phenomenon. While the train is moving toward the person, the person perceives the whistle as having a pitch (frequency) that is higher than the pitch that one on the train would perceive the whistle as having. But after the train passes the person, and is thus moving away from him, the person perceives the whistle as having a pitch lower than the pitch that one on the train would perceive the whistle as having.
Consequently, the subcarrier frequencies of the OFDM symbol 25 of FIG. 4 may be influenced by the Doppler Effect in a similar manner at the receiver of the client 12 of FIG. 3.
A measure of the influence that the Doppler Effect has on a single transmitted tone (e.g., an unmodulated subcarrier signal with constant, non-zero amplitude) is the “Doppler Spread”, which is the bandwidth that the tone may occupy at the receiver due to the Doppler Effect. For example, suppose that the frequency of the tone is 1,000 Hz at the transmitter, but that at the receiver, due to the non-zero velocity of the receiver relative to the transmitter, the received tone may have a frequency anywhere from 980 Hz to 1,020 Hz depending on the instantaneous velocity. Therefore, in this example, the Doppler Spread=1020 Hz−980 Hz=40 Hz. That is, the Doppler Spread is (40 Hz)/(1000 Hz)=4% of the frequency of the transmitted tone—although expressed here in Hz and as a percentage of the transmitted frequency, the Doppler Spread may be expressed in other quantities as described below.
For mobile OFDM devices, one may characterize the ICI caused by the Doppler Spread of a subcarrier in terms of the highest number of adjacent subcarriers with which the subcarrier may interfere. For example, the total Doppler induced ICI caused by the 50th (k=50) subcarrier is greater if energy from this subcarrier spills over to the 48th, 49th, 51st, and 52nd subcarriers, and is less if energy from this subcarrier spills over to only the 49th and 51st subcarriers. In actuality, because the Doppler Spread of a subcarrier may cause the subcarrier to spill over energy into many or all of the other N subcarrier slots to some degree, one may set a Doppler Spread interference threshold below which one subcarrier is deemed to be unaffected by the Doppler Spread of another subcarrier; such threshold may have units of, e.g., power or amplitude. Therefore, for a mobile OFDM device, the extent of Doppler induced ICI caused by a subcarrier k may be defined in terms of the number of adjacent subcarriers (above and below the subcarrier k in question) that may experience a level of ICI above the Doppler Spread interference threshold for the device. Furthermore, although in some applications one may assume that all of the subcarriers k experience the same Doppler Spread, in other applications, one may decide not to make this assumption.
Consequently, referring to FIGS. 3 and 4, the frequency slots 26 (only the frequency slot 26N-(a-4) of the subcarrier N−(a−4) is shown for clarity) each represent the bandwidth that a respective subcarrier transmitted by the base 10 may occupy at the receiving client 12 due to all causes (e.g., the existence of multiple transmission paths L, channel conditions, and Doppler Spread). But when the base 10 and client 12 are moving relative to one another, the greatest contributor to the frequency-slot bandwidth may be the Doppler Spread.
Still referring to FIGS. 3 and 4, because the Doppler Spread of an OFDM signal may vary relatively quickly with time, transmitting a training symbol separately from the data symbol may not allow the receiver of the client 12 to adequately determine the channel-estimation matrix Ĥ for the channel 14 as it exists while the OFDM data symbol is being transmitted.
Consequently, mobile OFDM devices, such as the base 10, may combine training subsymbols and data subsymbols into a single OFDM symbol such that a receiving device, such as the client 12, may characterize the channel 14 for the same time period during which the data subsymbols are transmitted.
FIG. 5 is a frequency plot of some of the N subcarriers k (here, subcarriers k=N−a to N−(a−12)) of an embodiment of an OFDM symbol 28, which may be transmitted by the base 10 of FIG. 3 and received by the client 12 of FIG. 3, or vice versa, where the OFDM symbol includes both training and data subsymbols. Although the base 10 is described as transmitting the OFDM signal in the example below, it is understood that this example would be similar if the client 12 were transmitting the OFDM signal.
The OFDM symbol 28 includes one or more clusters LD of data subcarriers, and one or more clusters LP of training subcarriers, which are hereinafter called “pilot” subcarriers. The transmitter of the base 10 may modulate the pilot subcarriers with respective pilot subsymbols. In an embodiment, the data clusters LD and the pilot clusters LP are arranged in alternating fashion (i.e., one after the other) such that each data cluster LD is separated from adjacent data clusters by at least one pilot cluster LP, and such that each pilot cluster is separated from adjacent pilot clusters by at least one data cluster) within the OFDM symbol 28. As discussed below in conjunction with FIGS. 9-10B, because the client 12 receiver “knows” the pilot subsymbols ahead of time, the client may use the pilot subsymbols to more accurately estimate the channel 14 as it exists while the data subsymbols are being transmitted.
In an embodiment, each data cluster LD within the OFDM symbol 28 includes a same first number (e.g., sixteen) of data subcarriers, and each pilot cluster LP within the OFDM symbol includes a same second number (e.g., five or nine) of pilot subcarriers. For example, in the embodiment of FIG. 5, the illustrated pilot cluster LP includes five pilot subcarriers k=N−(a−3) to N−(a−7), and the other pilot clusters (not shown in FIG. 5) of the OFDM symbol 28 also each include five respective pilot subcarriers. But in another embodiment, a data cluster LD may include a different number of data subcarriers than another data cluster within the same OFDM symbol, and a pilot cluster LP may include a different number of pilot subcarriers than another pilot cluster within the same OFDM symbol. Furthermore, as discussed above, some of the data subcarriers may be unmodulated by a data subsymbol or may have zero amplitude (i.e., zero energy), and, as discussed below in conjunction with FIGS. 7-8, some of the pilot subcarriers may be unmodulated by a pilot subsymbol or may have zero energy. Moreover, a pilot cluster LP or a data cluster LD may “wrap around the ends” of the N subcarriers. For example, if there are N=128 subcarriers (k=0 to 127), then a pilot cluster LP may include five pilot subcarriers k=126, k=127, k=0, k=1, and k=2.
A designer of an OFDM receiver, such as the receiver in the client 12 (FIG. 3), may select the minimum number NP of pilot clusters LP in the OFDM symbol 28, and may select the minimum number LPN of pilot subcarriers kP within each pilot cluster, for an intended application of the receiver based on the generally expected conditions of the communication channel 14 (FIG. 3) and on a desired data-error rate. For example, for an application where the receiver may be used in a moving automobile, a designer may use the generally expected conditions of a communication channel between a ground-based transmitter and receiver that are moving relative to one another at speeds between approximately 0 and 150 miles per hour (although non-racing automobiles rarely travel at speeds approaching 150 miles per hour, if the transmitter and receiver are in respective automobiles that are moving in opposite directions, then the speed of one automobile relative to the other automobile may approach or exceed 150 miles per hour). And to maximize the number of data subcarriers in, and thus the data bandwidth of, the OFDM symbol 28, the designer may select the minimum number NP of pilot clusters LP, and the minimum number LPN of pilot subcarriers kP within each pilot cluster, that he/she predicts will allow the receiver to estimate such a channel with an accuracy that is sufficient for the receiver to recover data within the desired error rate.
FIG. 6 is a frequency plot of some of the N subcarriers k of an embodiment of the OFDM symbol 28 of FIG. 5, where the frequency (x) axis of FIG. 6 has a lower resolution than the frequency (x) axis of FIG. 5.
In an embodiment, the pilot clusters LP are separated by a uniform separation value Psep, which is the distance, measured in the number of subcarriers k, between a pilot subcarrier in a pilot cluster and a corresponding pilot subcarrier in an adjacent pilot cluster. That is, a pilot subcarrier that occupies a relative position within a pilot cluster LP is Psep subcarriers away from a pilot subcarrier that occupies the same relative position within an adjacent pilot cluster. For example, as shown in FIG. 6, the center pilot subcarrier (relative position 0) in pilot cluster LPS is separated from the center pilot subcarrier (also relative position 0) in the pilot cluster LPS+1 by Psep subcarriers k. Also as shown in FIG. 6, the last pilot subcarrier (relative position +2 in this example) in LPS+1 is separated from the last pilot subcarrier (also relative position +2 in this example) in the pilot cluster LPS+2 by Psep subcarriers k. And, although not shown in FIG. 6, the very first pilot cluster LP0 in the OFDM symbol 28 is separated from the very last pilot cluster LP(Np-1) in the OFDM symbol by Psep when this separation is calculated modulo N—calculating such separations modulo N yields accurate separation values if a pilot cluster LP or a data cluster LD “wraps around the ends” of the N subcarriers as discussed above.
FIG. 7 is a frequency plot of an embodiment of a Frequency-Domain Kronecker Delta (FDKD) pilot cluster LPFDKD—S.
Before substantive characteristics of the pilot cluster LPFDKD—S are discussed, a convention for identifying a pilot cluster, such as the pilot cluster LPFDKD—S, and its pilot subcarriers is discussed. In this convention, Pb identifies the relative location of the center subcarrier within the pilot cluster, S identifies the relative location of the pilot cluster within an OFDM symbol, Wp is the total number of pilot subcarriers to the left and to the right of the center pilot subcarrier, Bp is the number of interior pilot subcarriers to the left and to the right of the center pilot subcarrier, and Wp−Bp is the number of guard pilot subcarriers Gp at each end of the pilot cluster. For example, if a pilot cluster LPFDKD—S includes LPN=5 total pilot subcarriers and two guard pilot subcarriers, then Wp=(5−1)/2=2, Bp=Wp−Gp=2−1=1, and the pilot cluster LPFDKD—S includes pilot subcarriers at the following relative locations: Pb−2, Pb−1, Pb, Pb+1, and Pb+2. And one may convert the relative-location identifiers into absolute-location identifiers by adding S·Psep to each of the relative-location identifiers. So, continuing with the above example, the pilot cluster LPFDKD—S includes pilot subcarriers at the following absolute locations: Pb+S·Psep−2, Pb+S·Psep−1, Pb+S·Psep, Pb+S·Psep+1, and Pb+S·Psep+2. And, therefore, again in this example, the pilot cluster LPFDKD—S includes the following pilot subcarriers: kPb+S·Psep−2, kPb+S·Psep−1, kPb+S·Psep, kPb+S·Psep+1, and kP b+S·Psep+2. For example, if each pilot cluster LPFDKD—S in an OFDM symbol includes LPN=5 pilot subcarriers, Psep=8, and the first pilot subcarrier of the zeroth pilot cluster LPFDKD—0 (S=0) is k0, then Pb=2, Wp=2, and the sixth pilot cluster LPFDKD—6 (S=6 and counting in a direction from the lowest to the highest subcarrier frequency) includes the following pilot subcarriers: k48, k49, k50, k51, and k52.
Still referring to FIG. 7, in an embodiment, the center subcarrier kPb+S·Psep (solid line in FIG. 7) of an FDKD pilot cluster LPFDKD—S is modulated with a non-zero pilot subsymbol, and all of the other subcarriers (dashed lines) have zero energy; that is, all of the other subcarriers are effectively modulated with a zero pilot subsymbol equal to 0+j0. Therefore, in a FDKD pilot cluster LPFDKD—S, the only energy transmitted within the pilot cluster LPFDKD—S is transmitted on the center subcarrier kPb+S·Psep; the remaining subcarriers in the pilot cluster are transmitted with zero energy. But for reasons discussed above in conjunction with FIG. 4, at the receiver, subcarriers of the pilot cluster LPFDKD—S other than the center subcarrier may carry non-zero energy due to Doppler Spread. And, as discussed below in conjunction with FIGS. 9-10, the energy carried by the interior pilot subcarriers at the receiver may allow the receiver to generate an estimate of the communication channel as it exists during transmission of an OFDM symbol, where the estimate takes into account ICI caused by Doppler Spread. The guard pilot subcarriers are included to provide a guard band that reduces to negligible levels the amount of energy from data subcarriers that “spills over” into the center and interior pilot subcarriers, and vice-versa. One may select the total number LPN of pilot subcarriers and the number GP of guard pilot subcarriers in a pilot cluster LP for a particular application based on the expected Doppler Spread. Typically, the larger the expected Doppler Spread, the larger the total number LPN of pilot subcarriers and the number Gp of guard pilot subcarriers, and the smaller the expected Doppler Spread, the smaller the total number LPN of pilot subcarriers and the number Gp of guard pilot subcarriers (Gp may even equal zero).
FIG. 8 is a frequency plot of an embodiment of an All-Pilot Pilot Cluster (APPC) LPAPPC—S. Unlike the FDKD pilot cluster LPFDKD—S of FIG. 7 in which only the center subcarrier kPb+S·Psep is modulated with a non-zero pilot subsymbol, in an APPC pilot cluster LPAPPC—S, all of the pilot subcarriers (solid lines) kPb+S·Psep−Wp−kPb+S·Psep+Wp are modulated with a respective non-zero pilot subsymbol. That is, energy is transmitted on all of the pilot subcarriers kPb+S·Psep−Wp−kPb+S·Psep+Wp within an APPC pilot cluster. Furthermore, the pilot subcarriers kPb+S·Psep−Wp−kPb+S·Psep+Wp of an APPC pilot cluster may each be modulated with the same, or with different, pilot subsymbols. And differences between the transmitted pilot subsymbols (which are known ahead of time by the receiver) and the respective received pilot subsymbols may allow the receiver to generate an estimate of the communication channel as it exists during transmission of an OFDM symbol, where the estimate takes into account ICI caused by Doppler Spread.
FIG. 9 is a block diagram of an embodiment of a receiver 30 for a mobile OFDM device such as the base 10 or client 12 of FIG. 3.
The receiver 30 includes a receive antenna 32, a Fast Fourier Transform (FFT) unit 34, a channel estimator 36, a data-recovery unit 38, and a decoder 40. The FFT unit 34, channel estimator 36, data-recovery unit 38, and decoder 40 may each be implemented in software, hardware, or a combination of software and hardware. For example, one or more of the FFT unit 34, the channel estimator 36, the data-recovery unit 38, and the decoder 40 may be implemented on an integrated circuit (IC), and other components, such as a transmitter, may also be implemented on the same IC, either on a same or different IC die. And this IC may be combined with one or more other ICs (not shown in FIG. 9) to form a system such as the base 10 or client 12 of FIG. 3. Or, one or more of these components may be implemented by a software-executing controller such as a processor.
The receive antenna 32 may receive one or more OFDM symbols from a transmitter, such as the transmitter of the base 10 or client 12 of FIG. 3, where at least some of the subcarrier signals may experience Doppler Spread. The antenna 32 may also function to transmit OFDM symbols generated by a transmitter (not shown in FIG. 9) of the OFDM device that incorporates the receiver 30. That is, the antenna 32 may function to both receive and transmit OFDM symbols.
The FFT unit 34 conventionally converts a received OFDM symbol from a time-domain waveform into an N×1 column vector y of complex frequency-domain coefficients (e.g., one complex coefficient for each subcarrier).
The channel estimator 36 estimates the response of the communication channel (e.g., the channel 14 of FIG. 3) from the coefficients of the vector y corresponding to the pilot subcarriers, which, as discussed above in conjunction with FIGS. 5-8, are the subcarriers that compose the training portion of the received OFDM symbol. From these pilot-subcarrier coefficients, the estimator 36 generates an N×N channel-estimation matrix Ĥ of complex frequency coefficients that collectively approximate the effective frequency response H of the communication channel—the effective frequency response may take into account the affect of, e.g., channel conditions such as temperature and humidity, the existence of multiple transmission paths, and the Doppler Spread, at each of the subcarrier frequencies fk. Because, as discussed above, the Doppler Spread may cause energy from one subcarrier to spill over into the frequency slot of another subcarrier at the receiver 30, the matrix Ĥ may not be a diagonal matrix—a matrix is diagonal if all of its elements are zero except for the elements that lie along the main diagonal that extends from the top left corner of the matrix. An embodiment of the channel estimator 36, and an embodiment of a technique for generating the channel-estimation matrix Ĥ, are discussed below in conjunction with FIG. 10.
The data-recovery unit 38 recovers the data carried by the OFDM symbol as transmitted by generating an N×1 column vector {circumflex over (x)}, which is an estimation of the transmitted OFDM data symbol. That is, {circumflex over (x)} includes complex coefficients (one for at least each data subcarrier) that are estimates of the complex coefficients with which the transmitter modulated the transmitted data subcarriers. The unit 38 may generally recover {circumflex over (x)} according to the following equations:

y=Ĥ{circumflex over (x)}+n  (1)

Ĥ−1(y)=Ĥ−1Ĥ{circumflex over (x)}+Ĥ−1n={circumflex over (x)}+Ĥ−1n  (2)

where n is an N×1 column vector of Additive-White-Gaussian-Noise (AWGN) complex coefficients at each of the subcarrier frequencies. Because, as discussed above, some of the y coefficients are for pilot subcarriers that are used only for channel-estimation purposes, the elements of Ĥ, {circumflex over (x)}, y, and n that correspond to the NpLPN pilot subcarriers (where Np is the number of pilot clusters Lp in the OFDM symbol and LPN is the number of pilot subcarriers per pilot cluster LP) may be discarded prior to calculating Ĥ−1 and solving equation (2) so as to reduce the complexity, and increase the speed, of the calculation of {circumflex over (x)}. Examples of a data-recovery unit and data-recovery techniques that may be used as and by the data-recovery unit 38 are disclosed in U.S. patent application Ser. Nos. 12/579,935 and 12/579,969, which were filed on Oct. 15, 2009 and which are incorporated by reference. And conventional data-recovery units and techniques that may be respectively used as and by the data-recovery unit 38 also exist.

The data decoder 40 effectively uses the {circumflex over (x)} coefficients that correspond to the data subcarriers of the OFDM symbol to demodulate the corresponding data subsymbols, and to thus recover the data represented by the subsymbols. For example, if the transmitter modulated a data subcarrier by mapping it to a respective QPSK constellation element, then the data decoder 40 QPSK demodulates the data subcarrier to recover the same constellation element, which represents the bits of data carried by the modulated data subcarrier.
Still referring to FIG. 9, although conventional channel estimators exist, such a channel estimator may require a relatively long processing time to determine the channel-estimation matrix Ĥ. For example, a significant portion of the processing time consumed by a conventional channel estimator may be due to the calculating of one or more inverted matrices in real time as part of the algorithm for determining Ĥ.
And referring to FIGS. 3 and 9, a conventional channel estimator may also be unable to account for changes in the number Z of the paths L that compose the communication channel 14, for changes in the respective delays of these paths, and for changes in the respective portions of the OFDM signal energy carried by these paths.
Over a period of time that may be much longer than a single OFDM symbol period (e.g., approximately 100-300 OFDM symbol periods), the number Z of paths L may change. The change in the number of paths L may be due to changes in the channel conditions, such as changes in the number of OFDM-signal-reflecting objects within or near the channel 14.
Furthermore, over the same period, the delays of the paths L, and the portions of the OFDM signal energy carried by the paths L, may also change. Each path L is defined by the delay it has relative to the zeroth path L0 having zero delay. That is, the zero-delay path L0 is the path over which a version of an OFDM signal, having a respective portion of the energy of the transmitted OFDM signal, first reaches the receiver; other versions of the OFDM signal reach the receiver over the remaining paths L at the respective delay times (relative to the delay of the path L0) that define those paths, and with respective portions of the transmitted energy. The delay time of a path L may be defined in units of the OFDM-signal sampling time employed by the receiver. For example, when a version of an OFDM signal propagates over a path Ll having a delay value of 1.0, this signal version first reaches the receiver one sample time, or one sample, after the version of the OFDM signal that is propagating over the path L0 first reaches the receiver. Likewise, when a version of an OFDM signal propagates over a path Ll having a delay value of 3.5 samples, this signal version first reaches the receiver three-and-one-half samples after the version of the OFDM signal that is propagating over the path L0 first reaches the receiver. To account for these delayed one or more paths L, the transmitter (not shown in FIG. 9) may add a cyclic prefix to the transmitted signal, where this prefix includes a number of samples, the aggregate delay of which is at least as long as the longest path delay. For example, if the path L with the longest delay has a delay of 3.5 samples, then the transmitter may add a cyclic prefix of four samples to the transmitted signal, such that the transmitted signal includes N+4 samples (as above, N is the total number of transmitted subcarriers k). These four extra samples are actually the last four samples of the signal to be transmitted, and are effectively repeated at the beginning of the signal transmission to be sure that by the time that the last signal sample arrives at the receiver over the zeroth-delay path L0, the receiver has also received over the remaining paths all of the samples of the signal at least one time (because the signal is a periodic time-domain signal, receiving a sample of the signal more than one time typically has no negative affect at the receiver).
Unfortunately, a channel estimator that does not account for changes in at least one of the number, delays, and energies of the paths L may be unable to determine the channel-estimation matrix Ĥ with an accuracy sufficient for some applications such as mobile OFDM.
FIG. 10 is a block diagram of the channel estimator 36 of FIG. 9, where the channel estimator may determine the channel-estimation matrix Ĥ recursively, without calculating the inverse of a matrix in real time (or otherwise), and by accounting for changes in the number, delays, and/or energies of the paths L that compose the communication channel 14 (FIG. 3).
The estimator 36 includes a first stage 50 for determining path-independent quantities, b parallel second stages 520-52b-1 for respectively determining column vectors hl(s) that describe the time-domain response of the Z paths L of the channel 14 (FIG. 3) during a symbol period s, a communication-path monitor 54 for monitoring the number and delays of the channel paths L, and a channel-matrix calculator 56 for determining the channel-estimation matrix Ĥ(s) for the symbol period s.
The first stage 50 determines quantities that are independent of any particular channel path L, and that may be used by the second and third stages 52 and 56. Examples of, and techniques for determining, such quantities are discussed below.
Each of the second stages 52 determines a respective time-domain path vector hl(s) for a respective one of the Z paths l=L0−l=Lz-1. The number b of second stages 52 depends on the path delays that the channel 14 (FIG. 3) may possibly have for a particular application. For example, suppose that even though it is anticipated that the channel 14 will not have more than Z=4 simultaneous paths L during a symbol period s, the delays of these paths may range from 0 to 4 samples in increments of 0.25 samples, for a total of 4×1/(0.25)=16 possible path delays. Therefore, in such an example, the channel estimator 36 would include b=16 second stages 520-5215, one stage for each of the anticipated sixteen path delays, respectively. As discussed below, the path monitor 54 engages the second stages 52 corresponding to the delays of the paths L present in the channel 14.
Each second stage 52 includes a first substage 58, a second substage 60, a third substage 62, and an engage/disengage switch 64.
Each first substage 58 is for determining quantities that are dependent on the particular channel path L associated with the second stage, and that may be used by the corresponding second substage 60. Examples of, and techniques for calculating, such quantities are discussed below.
Each second substage 60 may include a respective recursive filter, such as a Vector State Scalar Observation (VSSO) Kalman filter, which may increase the accuracy of the respective determined vector hl(s) without increasing the complexity (or even reducing the complexity) of the channel estimator 36 as compared to prior channel estimators. The recursive-filter substage 60 may increase the accuracy of hl(s) by effectively using information from preceding symbol periods to determine his) for a current symbol period s. For example, referring to FIG. 3, suppose that the client 12 is moving at an approximately constant velocity relative to the base 10; therefore, from symbol period to symbol period, one would expect the Doppler Spread to be approximately the same. Without the recursive-filter substage 60, the second stage 52 may allow an anomaly, such as a noise “spike,” during a symbol period s to introduce a significant error into the path vector hl(s), because the second stage has no way to “know” that the Doppler Spread is approximately constant relative to prior symbol periods. But because the recursive-filter substage 60 may track the trend (e.g., approximately constant Doppler Spread) of the response of the path L, it may allow the second stage 52 to lessen, or even eliminate, the error that an anomaly may introduce into hl(s). Furthermore, one may design the recursive-filter stage 60 such that it does not perform a matrix inversion; for example, a VSSO Kalman filter may be designed so that it does not perform a matrix inversion. This may reduce the complexity of each second stage 52, and thus may reduce the overall complexity of the channel estimator 36 as compared to conventional channel estimators. An embodiment of a recursive-filter substage 60 is described below.
Each third substage 62 determines the respective path vector hl(s) in response to the second substage 60 as described below.
The communication-path monitor 54 tracks changes to the number, delays, and energies of the communication paths L, and periodically adjusts which of the second stages 52 are engaged and disengaged based on the delays and numbers of paths L that are currently present in the channel 14 (FIG. 3). For example, if the path monitor 54 determines that the channel 14 currently has Z=4 active paths L having relative delays of 0.0 (the zero-delay path typically is always present), 0.25, 1.25, and 2.0 respectively, then the path monitor engages the second stages 52 corresponding to these delays via respective switches 64, and disengages the remaining second stages via respective switches 64. The path monitor 54 determines which paths are active (i.e., present for purposes of the receiver 30 of FIG. 9) by monitoring the energies of the paths and comparing the energies to a path threshold. If a path's energy is greater than the threshold, then the corresponding path is active/present; otherwise, the corresponding path is inactive/not present. An embodiment of the path monitor 54 is further described in U.S. patent application Ser. No. 12/963,569, which is incorporated by reference.
The third stage 56 generates the channel-estimation matrix Ĥ in response to the path vectors hl(s) from the second stages 52 that the communication-path monitor 54 engages.
An embodiment of the second recursive-filter substage 600 of the second stage 520 is now described where the substage 600 includes a VSSO Kalman filter, it being understood that the second substages 601-60b-1 may be similar.
The VSSO-Kalman-filter substage 600 includes an observation scalar calculator 660, a state-vector predictor 680, a mean-square-error-matrix predictor 700, a gain-vector calculator 720, a state-vector estimator 740, a mean-square-error-matrix updater 760, and a scaling-vector calculator 780; these components are described below.
Before describing the operation of an embodiment of the channel estimator 36 of FIG. 10, some channel-estimation-related quantities, and the mathematical relationships between some of these quantities, are described. All of the quantities and relationships described below assume that APPC pilot clusters (each including the same pilot symbol from pilot subcarrier to pilot subcarrier and from pilot cluster to pilot cluster as discussed above in conjunction with FIG. 8) are used unless otherwise noted.

hl(s)=[hl(s), . . . ,hl(s+N−1)]T  (3)

where hl(s) is the column vector that represents the time-domain response of the path l=L during the sth OFDM symbol period, s is the first sample time after the cyclic prefix (if there is a cyclic prefix) in the sth OFDM symbol period, and N is the number of subcarriers k (both pilot and data subcarriers) in the transmitted OFDM signal. For example, if N=128, s=1 (2nd OFDM symbol), and the cyclic prefix has four samples, then the transmitted OFDM signal carrying the 2nd OFDM symbol has a total of 128+4=132 samples, s represents the 268th sample time (where the sample times are numbered continuously starting with the 1st OFDM symbol s=0), and hl(s) includes one hundred twenty eight complex elements corresponding to the samples 268-395.
In at least some applications, the elements of hl(s) may be approximated as fitting a curve such as a straight line. Therefore, the elements of hl(s) may be represented in terms of a polynomial that describes the curve. For example, where the curve is a straight line, which one may represent with the equation y=mx+b where m is the slope of the line and b is the y-axis intercept, hl(s) may be similarly represented in terms of an offset and slope according to the following equation:

hl(s)=B hl(s)  (4)

where B is a binomial expansion matrix having elements m, n arranged in Q columns such that B(m,n)=mn (m is the row number and n is the column number), and hl(s) is a scaling column vector having Q rows/elements; consequently, where the fitting curve is a straight line,





  B
  =
  
    [
    
      
        
          1
        
        
          0
        
      
      
        
          ⋮
        
        
          ⋮
        
      
      
        
          1
        
        
          
            N
            -
            1
          
        
      
    
    ]
  




and hl(s) is a column vector with Q=2 elements that respectively represent offset and slope. Because typically Q<<N, hl(s) is typically much smaller, and easier to manipulate, than hl(s).

The state vector gl(S) for the engaged filter substage 60 corresponding to the lth path during the symbol period s is given by the following equation:

gl(S)=[ hl(s−M+1)T, . . . , hl(s)T]T  (5)

where M, an integer, is the filter prediction order that provides a filter substage 60 with its recursive feature. For example, to design a filter substage 60 for calculating the state vector gl(S) using information from the current symbol period and the previous three symbol periods, a designer would set M=4. Generally, the higher the prediction order M, the more accurate the filter substage 60 but the longer its latency; conversely, the lower the value of M, generally the less accurate the filter substage, but the shorter the latency.

The state equation for the engaged filter substage 60 corresponding to the lth path relates the lth path during the current symbol period s to the same lth path during one or more prior symbol periods, and is as follows:

gl(S)=Agl(s-1)+el(s)  (6)

where A is an autoregressive matrix and e is the prediction-error vector. A is dependent on the Doppler Spread, and, therefore, the first stage 50 may determine values of A ahead of time in a conventional manner and store these values in a lookup table (e.g., part of the first stage 50 or external thereto), which the first stage may access based on the velocity of the receiver relative to the transmitter; for example, the receiver may determine this velocity using a GPS device. Alternatively, the channel estimator 36 may include a conventional linear-adaptive filter (not shown in FIG. 10) that conventionally looks at the pilot symbols recovered by the receiver for one or more prior symbol periods, predicts the pilot symbols to be recovered for the current symbol period s based on the current velocity of the receiver relative to the transmitter, and predicts the value of the A matrix based on the previously recovered pilot symbols and the predicted pilot symbols.

The prediction-error-correlation matrix Gl is given by the following equation:

Gl=E{el(s)el(s)H}  (7)

Although the vector el(s) may be unknown, its expectation (the right side of equation (7)), which may be generally described as an average of the change in the variance of el(s) from symbol period to symbol period, depends on the Doppler Spread, and, therefore, may be conventionally determined ahead of time through simulations or with a closed-form expression; because this expectation is the same from symbol period s to symbol period s, Gl does not depend on s. Consequently, the first substage 58 may determine values for Gl dynamically or ahead of time, and/or store these values of Gl in a lookup table with respect to Doppler Spread, and may retrieve from the lookup table a value of Gl for the current symbol period based on the velocity of the receiver relative to the transmitter during the current symbol period.

A path-dependent 1×(2wp+1) row vector ul, which the first substage 58 may calculate and/or store dynamically or ahead of time, is given by the following equation:




  
    
      
        
          u
          1
        
        =
        
          {
          
            
              e
              
                -
                
                  
                    j2π
                    ⁢
                    
                      
                    
                    ⁢
                    
                      w
                      p
                    
                    ⁢
                    l
                  
                  N
                
              
            
            ⁢
            
              e
              
                -
                
                  
                    j2π
                    ⁢
                    
                      
                    
                    ⁢
                    
                      (
                      
                        
                          w
                          p
                        
                        ⁢
                        1
                      
                      )
                    
                    ⁢
                    l
                  
                  N
                
              
            
            ⁢
            ...
            ⁢
            
              
            
            ⁢
            1
            ⁢
            ...
            ⁢
            
              
            
            ⁢
            
              e
              
                
                  j2π
                  ⁢
                  
                    
                  
                  ⁢
                  
                    w
                    p
                  
                  ⁢
                  l
                
                N
              
            
          
        
      
    
    
      
        (
        8
        )
      
    
  




A path-independent matrix W, which the first stage 50 may calculate and/or store dynamically or ahead of time, is given by the following equation:




  
    
      
        W
        =
        
          [
          
            
              
                
                  
                    F
                    H
                  
                  ⁡
                  
                    (
                    
                      
                        〈
                        
                          N
                          +
                          
                            w
                            p
                          
                        
                        〉
                      
                      ,
                      
                        :
                      
                    
                    )
                  
                
              
            
            
              
                
                  
                    F
                    H
                  
                  ⁡
                  
                    (
                    
                      
                        〈
                        
                          N
                          +
                          
                            w
                            p
                          
                          -
                          1
                        
                        〉
                      
                      ,
                      
                        :
                      
                    
                    )
                  
                
              
            
            
              
                ⋮
              
            
            
              
                
                  
                    F
                    H
                  
                  ⁡
                  
                    (
                    
                      
                        〈
                        
                          N
                          -
                          
                            w
                            p
                          
                        
                        〉
                      
                      ,
                      
                        :
                      
                    
                    )
                  
                
              
            
          
          ]
        
      
    
    
      
        (
        9
        )
      
    
  




where F is the known Fourier matrix, the “” operator indicates a modulo N operation, and “:” indicates all columns of the matrix FH in the indicated rows. Note that the number of rows in the W matrix is equal to the number of pilot subcarriers LPN in each transmitted/received pilot cluster Lp.

A path-dependent 1×(MQ) row vector qlH, which the first substage 58 may calculate and/or store dynamically or ahead of time, is given by the following equation:




  
    
      
        
          q
          l
          H
        
        =
        
          
            
              PN
              p
            
            N
          
          ⁡
          
            [
            
              
                0
                
                  1
                  ⁢
                  
                    x
                    ⁡
                    
                      (
                      
                        M
                        -
                        1
                      
                      )
                    
                  
                  ⁢
                  Q
                
              
              ⁢
              
                
              
              ⁢
              
                u
                l
              
              ⁢
              WB
            
            ]
          
        
      
    
    
      
        (
        10
        )
      
    
  




where P is the pilot symbol (which is mapped to all pilot subcarriers in an embodiment) in the frequency domain, and 01x(M-1)Q is a row vector having (M−1)Q columns/elements that are each equal to zero.

A path-independent NP×Z Fourier matrix FL, which the first stage 50 may calculate and/or store dynamically or ahead of time for the expected values of Z, is given by the following equation:

FL=F(p(0),0:Z−1)  (11)

where “p(0)” indicates that FL includes the NP rows of the Fourier matrix F corresponding to the positions of the center pilot subcarriers of the pilot clusters Lp in the transmitted/received OFDM symbol, and “0:Z−1” indicates that FL includes columns 0-Z−1 of F, where Z is the number of paths L present in the channel during the symbol period s.

The observation scalar yl(s) for the engaged filter substage 60 corresponding to the lth path is given by the following equation:

 yl(s)=FLH(l,:)y(s)(p(0))  (12)

where y(s) is the received-signal column vector in the frequency domain during the symbol period s, and “p(0)” indicates that y(s)(p(0)) includes only the elements of y(s) that correspond to the center pilot subcarriers of the transmitted/received pilot clusters Lp. Although here only the center subcarrier of each pilot cluster is used to generate yl(s), other embodiments may use different and/or more subcarriers within each pilot cluster to generate yl(s).

The measurement equation for the engaged filter substage 60 corresponding to the lth path is given by the following equation:

 yl(s)=qlHgl(s)+ nl(s)  (13)

where nl is the noise due to, e.g., interference on the pilot subcarriers from the data subcarriers and Additive White Gaussian Noise (AWGN). Although nl(s) may be unknown ahead of time, the first substage 58 associated with the lth path may compute its expectation/variance σl2=E{| nl(s)|2} dynamically or ahead of time by simulation or as a closed-form expression in a conventional manner, and may use σl2 as described below.

Referring to equation (12) and as further discussed below, the measurement equation effectively relates the symbol recovered during the symbol period s to the channel response during s, and, referring to equation (13) and also as further discussed below, the state equation (6), via the state vector gl(s), effectively modifies the result yl(s) given by the measurement equation (12) based on the channel response during one or more prior symbol periods. Furthermore, because yl(s) is a scalar, as discussed below, the filter substage 60 does not invert a matrix, which significantly reduces the overall complexity of the channel estimator 36 as compared to conventional channel estimators.
Still referring to FIG. 10, the operation of an embodiment of the channel estimator 36 is described in terms of the second stage 520, it being understood that the operations of the other second stages 52 may be similar. Furthermore, in an embodiment, at least one path L having a relative delay of zero is always present in the channel 14 (FIG. 3), and the second stage 520 is designed to determine hl=0(s) for the l=L0=0 path having a delay of zero; therefore, in such an embodiment, the path monitor 54 always engages the second stage 520 for the path l=L0=0 having a delay of zero. Moreover, in the example below, the elements of hl(s) are fitted to a straight line as described above.
First, the path monitor 54 determines the number Z and corresponding delays of the paths L that compose the channel 14 (FIG. 3), and engages, via the switches 64, the second stages 52 that correspond to these paths. As discussed above, for purposes of the following example, it is assumed that the path monitor 54 has engaged at least the second stage 520.
Next, the first stage 50 may determine and/or store quantities (at least some of which are described above) that the second stage 520 may need for its calculations, to the extent that the first stage has not already determined and/or stored these quantities.
Similarly, the first substage 580 may determine and/or store quantities (at least some of which are described above) that the filter substage 600 may need for its calculations, to the extent that the first substage has not already determined and/or stored these quantities.
Next, the observation-scalar calculator 660 determines the observation scalar yl(s) for l=0 according to equation (12).
Then, the state-vector predictor 680 determines the predicted state vector l(s) for l=0 according to the following equation:

l(s)=Aĝl(s-1)  (14)

Where s=0 (the initial symbol period), the predictor 680 also provides an initial value for ĝl(−1). This initial value may be zero, or it may be the expectation of ĝl(−1). If the initial value is the latter, the predictor 680 may compute the expectation of ĝl(−1) dynamically or ahead of time and store the computed expectation. A technique for calculating the expectation of ĝl(−1) is described in S. M. Kay, “Fundamentals of Statistical Signal Processing: Estimation Theory,” Prentice Hall: New Jersey (1993), which is incorporated by reference. After the initial symbol period s=0, the state-vector estimator 740 provides ĝl(s), which becomes ĝl(s-1) for the next symbol period s as discussed below.

Next, the mean-square-error-matrix predictor 700 determines the predicted mean-square-error matrix l(s) for l=0 according to the following equation:

l(s)=A{circumflex over (θ)}l(s-1)AH+Gl  (15)

Where s=0 (the initial symbol period), the predictor 700 also provides an initial value for {circumflex over (θ)}l(−1). This initial value may be zero, or it may be the expectation of the error variance in the state equation (6). If the initial value is the latter, then the predictor 700 may compute the expectation of the error variance in the state equation dynamically or ahead of time store the computed expectation. A technique for calculating the expectation of the error variance in the state equation (6) is described in S. M. Kay, “Fundamentals of Statistical Signal Processing: Estimation Theory,” Prentice Hall New Jersey (1993), which is incorporated by reference. After the initial symbol period s=0, the mean-square-error-matrix updater 760 provides {circumflex over (θ)}l(s), which becomes {circumflex over (θ)}l(s-1) for the next symbol period s as discussed below.

Then, the gain-vector calculator 720 determines a gain vector Ωl(s) for l=0 according to the following equation:




  
    
      
        
          Ω
          l
          
            (
            s
            )
          
        
        =
        
          
            
              
                θ
                 ̆
              
              l
              
                (
                s
                )
              
            
            ⁢
            
              q
              l
            
          
          
            
              
                σ
                _
              
              l
              2
            
            +
            
              
                q
                l
                H
              
              ⁢
              
                
                  θ
                   ̆
                
                l
                
                  (
                  s
                  )
                
              
              ⁢
              
                q
                l
              
            
          
        
      
    
    
      
        (
        16
        )
      
    
  




Next, the state-vector estimator 740 generates the estimated state vector ĝl(s) for l=0 according to the following equation:

ĝl(s)=l(s)+Ωl(s)[ yl(s)−qlHl(s)]  (17)

As discussed above, ĝl(s-1) is fed back to the state-vector predictor 680 to be used in equation (14) as ĝl(s-1) for the next symbol period.

Then, the mean-square-error-matrix updater 760 generates an updated mean-square-error matrix {circumflex over (θ)}l(s) for l=0 according to the following equation:

{circumflex over (θ)}l(s)=[IMQ−Ωl(s)qlH]l(s)  (18)

where IMQ is an identity matrix of dimensions M(row)×Q(column). Furthermore, as discussed above, {circumflex over (θ)}l(s) is fed back to the mean-square-error-matrix predictor 700 to be used in equation (15) as {circumflex over (θ)}l(s-1) for the next symbol period.

Next, the scaling-vector calculator 780 determines the scaling vector hl(s) for l=0 and for a straight-line approximation of the elements of hl(s) according to one of the two following equations:

 hl(s)=ĝl(s)(MQ−Q:MQ−1)  (19)

 hl(s-M)=ĝl(s)(0:Q−1)  (20)

Equation (19) may be referred to as the normal Kalman filter (NKF) output, and equation (20) may be referred to as the Kalman fixed-lag smoother (KFLS) output, which is effectively a low-pass filtered output. Generally, the KFLS output is more accurate, but has a higher latency, than the NKF output.

Then, the third stage path-vector calculator 620 determines the path vector hl(s) for l=0 according to equation (4) using either hl(s) from equation (19) or hl(s-M) from equation (20).
As stated above, the other engaged second stages 52 may operate in a similar manner to generate hl(s) for the paths L1≦l≦LZ-1 to which they correspond. Typically, all engaged second stages 52 generate hl(s) according to equation (19) or equation (20) for a symbol period s, although it is contemplated that some second stages may generate hl(s) according to equation (19) while other second stages may generate hl(s) according to equation (20) for a symbol period s.
Next, the third stage channel-matrix calculator 56 generates an intermediate channel-estimation matrix Ĥ(s) from the path-response vectors hl(s) for all of the paths L0≦l≦LZ-1 that compose the channel 14 (FIG. 3) according to the following equation:

Ĥ(s)(m,n)=ĥ(m-n)(s)(s+m), for 0≦m≦N−1 and 0≦n≦N−1  (21)

Then, the third stage channel-matrix calculator 56 generates the channel-estimation matrix Ĥ(s) according to the following equation:




  
    
      
        
          
            H
            ^
          
          
            (
            s
            )
          
        
        =
        
          
            1
            N
          
          ⁢
          F
          ⁢
          
            
              
                H
                _
              
              ^
            
            
              (
              s
              )
            
          
          ⁢
          
            F
            H
          
        
      
    
    
      
        (
        22
        )
      
    
  




Still referring to FIG. 10, alternate embodiments of the channel estimator 36 are contemplated. For example, the functions contributed to any of the components of the channel estimator 36 may be performed in hardware, software, or a combination of hardware and software, where the software is executed by a controller such as a processor. Furthermore, although described as VSSO Kalman filters, one or more of the second substages 60 may be another type of recursive filter, for example, another type of recursive filter that is designed to perform no matrix inversions. Moreover, although described as operating in response to APPC pilot clusters (FIG. 9), the channel estimator 36 may be modified (e.g., by modifying some or all of the above equations according to known principles) to operate in response to FDKD pilot clusters (FIG. 8). Furthermore, instead of, or in addition to, disengaging the unused second stages 52, the path monitor 54 may cause these unused second stages to enter a low- or no-power mode to save power.
Referring to FIGS. 1-10, as discussed above, an OFDM system such as shown in FIG. 3 forms a single multipath channel 14 between a single antenna of the base 10 and a single antenna of client 12, where during each OFDM symbol period, the transmitting one of the base and client transmits one OFDM symbol over this channel.
To increase the data-transmission rate relative to an OFDM system such as described above in conjunction with FIGS. 1-10, engineers have developed a Multiple-Input-Multiple-Output (MIMO)-OFDM system that forms multiple channels between the base and client, where, during each symbol period, the transmitting one of the base and client transmits a respective OFDM symbol from each of multiple transmit antennas using the same N data and pilot subcarriers. For example, if a MIMO-OFDM system uses three transmit antennas, then, for a given symbol period and value for N, the MIMO-OFDM system may transmit data at approximately three times the rate at which an OFDM system may transmit data, and may do this using approximately the same bandwidth! And even though the MIMO-OFDM symbols include the same subcarrier-frequencies, a phenomenon called “spatial diversity” may allow the receiver to recover all of the transmitted symbols with an error rate that is suitable for many applications.
FIG. 11 is a diagram of a MIMO-OFDM system 90, which includes a base transmitter-receiver 92 and a client transmitter-receiver 94; the diagram is simplified to include only the antennas 96 and 98 of the base and client, respectively. Furthermore, only the configuration/operation of the system 90 where the base 92 is the transmitter and the client 94 is the receiver is discussed, it being understood that the configuration/operation of the system where the client is the transmitter and the base is the receiver may be similar. Moreover, in the described configuration of the system 90, although the client 94 may include more than one antenna 98, it uses only one antenna for receiving signals from the base 92. In addition, the base 92 and client 94 may be moving relative to one another such that signals propagating between the base and client may experience Doppler Spread.
The base 92 includes T antennas 960-96T-1, and, in a transmitting configuration, transmits a respective OFDM signal carrying a respective OFDM symbol via each of these T antennas during a symbol period s, where, as discussed above, each OFDM signal includes the same N subcarriers. The combination of these simultaneous T OFDM signals may be referred to as a MIMO-OFDM signal. Furthermore, the base 92 may include a respective transmitter for each antenna 96, or may include fewer than T transmitters, at least some of which drive multiple ones of the antennas 96.
Therefore, in the described configuration, the system 90 forms T multipath transmit channels 1000-100T-1 between the respective transmit antennas 960-96T-1 and the receive antenna 98. That is, the system 90 forms a respective channel 100 between each transmit antenna 960-96T-1 and the single receive antenna 98. Furthermore, in an embodiment, the system 90 “assumes” that each channel 100 has the same number Z of paths L.
Consequently, for a given symbol period s and number N of subcarriers, the MIMO-OFDM system 90 may transmit data at rate that is approximately T times the rate at which an OFDM system transmits data.
Because the channels 100 each include different paths L, the channels may be said to be spatially different or diverse. As discussed above and as evident from the equations discussed below in conjunction with FIG. 14, even though the base 92 transmits the T OFDM signals using the same N subcarriers, the spatial diversity of the channels 100 allows the client 94 to recover each of the transmitted symbols with an error rate that may be suitable for many applications, for example, mobile applications where Doppler Spread may be present.
FIG. 12 is a diagram of a MIMO-OFDM system 110, which includes a base transmitter-receiver 112 and a client transmitter-receiver 114; the diagram is simplified to include only the antennas 116 and 118 of the base and client, respectively. Furthermore, only the configuration of the system 110 where the base 112 is the transmitter and the client 114 is the receiver is discussed, it being understood that the configuration of the system where the client is the transmitter and the base is the receiver may be similar. In addition, the base 112 and client 114 may be moving relative to each other such that signals propagating between the base and client may experience Doppler Spread.
A difference between the MIMO-OFDM system 110 and the MIMO-OFDM system 90 of FIG. 11 is that in the system 110, the client 114 includes and uses R>1 antennas 118 to receive the OFDM signals that the base 112 respectively transmits via the T transmit antennas 116; consequently, the system 110 forms T×R channels 120. In an embodiment of the system 110, R≧T−1.
Although the multiple receive antennas R may not increase the data rate, they may increase the robustness of the system 110. For example, although each receive antenna 118 receives the same T OFDM signals from the transmit antennas 116, each receive antenna receives these T signals over channels that are spatially diverse relative the channels over which the other receive antennas receive these signals. Therefore, although the OFDM signals received by one receive antenna 118 may carry OFDM symbols that are redundant relative to the OFDM symbols carried by the OFDM signals received by the other receive antennas, the spatial diversity of the channels over which the receive antennas receive this redundant information may decrease the data error rate because the client 114 has more diverse channels and paths from which to recover the T OFDM symbols. Furthermore, if one or more of the channels 120 between the transmit antennas 116 and one of the receive antennas 118 experiences catastrophic fading or other interference at a frequency of one or more of the N subcarriers, then the client 114 may still be able to recover the T transmitted OFDM symbols via one or more of the other receive antennas that receive the T OFDM signals over uncorrupted channels.
FIG. 13 is a block diagram of an embodiment of a receiver 130 for a mobile MIMO-OFDM device such as the base 92 or client 94 of FIG. 11, and such as the base 112 or client 114 of FIG. 12.
The receiver 130 includes R receive antennas 1320-132R-1, R FFT units 1340-134R-1, a received-signal combiner 136, a channel estimator 138, a data-recovery unit 140, and a decoder 142. The FFT units 134, combiner 136, channel estimator 138, data-recovery unit 140, and decoder 142 may each be implemented in software, hardware, or a combination of software and hardware. For example, one or more of these items may be implemented on an integrated circuit (IC), and other components, such as a transmitter, may also be implemented on the same IC, either on a same or different IC die. And this IC may be combined with one or more other ICs (not shown in FIG. 13) to form a system such as the MIMO-OFDM system 90 of FIG. 11 or the MIMO-OFDM system 110 of FIG. 12. Alternatively, the functions of one or more of these components may be performed by a controller, such as a processor, executing software instructions.
Each of the receive antennas 132 may receive OFDM singles from multiple transmit antennas, such as the T transmit antennas 96 of FIG. 11 or the T transmit antennas 116 of FIG. 12, where at least some of the N subcarrier signals may experience Doppler Spread. The receive antennas 132 may also function to transmit collectively a MIMO-OFDM signal generated by a transmitter (not shown in FIG. 13) of the MIMO-OFDM device that incorporates the receiver 130. That is, the antennas 132 may function to both receive and transmit MIMO-OFDM signals.
Each of the FFT units 1340-134R-1 conventionally converts a respective received MIMO-OFDM signal from a respective time-domain waveform into a respective N×1 column vector y0(s)-yR-1(s) of complex frequency-domain coefficients (e.g., one complex coefficient for each subcarrier).
The combiner 136 combines the vectors y0(s)-yR-1(s) into a single vector y(s). But if the device 130 has only R=1 receive antennas 132, then the combiner 136 may be omitted, and the output of the single FFT unit 1340 may be coupled to the y(s) input of the data-recovery unit 140. An embodiment of the combiner 136 is discussed below in conjunction with FIG. 16.
The channel estimator 138 estimates the responses of all of the communication channels (e.g., the channels 1000-100T-1 of FIG. 11 or the channels 1200-120TR-1 of FIG. 12) from the coefficients of the vectors y0(s)-yR-1(s) corresponding to the pilot subcarriers, which, as discussed above in conjunction with FIGS. 5-8, are the subcarriers that compose the training portion of the received MIMO-OFDM symbol. From these pilot-subcarrier coefficients, the estimator 138 generates an N×NR matrix Ĥ(s) of complex frequency coefficients that collectively approximate the effective frequency response H(s) of all the communication channels combined—the effective frequency response may take into account the affect of, e.g., channel conditions such as temperature and humidity and the Doppler Spread at each of the subcarrier frequencies fk in each of the channels, and the existence of multiple transmission paths per channel. Because, as discussed above in conjunction with FIGS. 3-8, the Doppler Spread may cause energy from one subcarrier to spill over into the frequency slot of another subcarrier at the receiver 130, the matrix Ĥ(s) may not be a diagonal matrix—a matrix is diagonal if all of its elements are zero except for the elements that lie along the main diagonal that extends from the top left corner of the matrix. An embodiment of the channel estimator 138, and an embodiment of a technique for generating the channel-estimation matrix Ĥ(s), are discussed below in conjunction with FIGS. 14-15.
The data-recovery unit 140 recovers the data carried by the MIMO-OFDM symbol as transmitted by generating a TN×1 column vector {circumflex over (x)}(s), which is an estimation of the transmitted MIMO-OFDM symbol, which is equivalent to T OFDM symbols. That is, {circumflex over (x)}(s) includes complex coefficients (one for at least each data subcarrier) that are estimates of the complex coefficients with which the transmitter(s) modulated the transmitted subcarriers. The unit 140 may generally recover {circumflex over (x)}(s) according to equations (1) and (2) above. Because, as discussed above in conjunction with FIGS. 3-8, some of the y(s) coefficients are for pilot subcarriers that are used only for channel-estimation purposes, the elements of Ĥ(s), {circumflex over (x)}(s), y(s), and n(s) that correspond to the TNpLPN pilot subcarriers (where TNp is the number of pilot clusters Lp in the MIMO-OFDM symbol, and LPN is the number of pilot subcarriers within each pilot cluster Lp) may be discarded prior to calculating Ĥ(s)−1 and solving equation (2) so as to reduce the complexity, and increase the speed, of the calculation of {circumflex over (x)}(s). Examples of a data-recovery unit 140 and data-recovery techniques that may be used as and by the data-recovery unit are disclosed in U.S. patent application Ser. Nos. 12/579,935 and 12/579,969, which were filed on Oct. 15, 2009 and which are incorporated by reference. And conventional data-recovery units and techniques that may be respectively used as and by the data-recovery unit 140 also exist.
The data decoder 142 effectively uses the {circumflex over (x)}(s) coefficients that correspond to the data subcarriers of the MIMO-OFDM symbol to demodulate the corresponding data subsymbols, and to thus recover the data represented by the subsymbols. For example, if a transmitter modulated a data subcarrier by mapping it to a respective QPSK constellation element, then the data decoder 142 QPSK demodulates the data subcarrier to recover the same constellation element, which represents the bits of data carried by the modulated data subcarrier.
Still referring to FIG. 13, although conventional MIMO-OFDM channel estimators exist, such a channel estimator may require a relatively long processing time to determine Ĥ(s). For example, a significant portion of the processing time consumed by a conventional channel estimator may be due to the calculating of one or more inverted matrices in real time as part of the algorithm for determining Ĥ(s).
And referring to FIGS. 11, 12, and 13, and as discussed above in conjunction with FIG. 9, a conventional channel estimator may also be unable to account for changes in the number of the paths L that compose the communication channels 100 or 120, for changes in the respective delays of these paths, and for changes in the respective portions of the MIMO-OFDM signal energy carried by these paths.
Unfortunately, a channel estimator that does not account for changes in at least one of the number, delays, and energies of the paths L may be unable to determine the channel-estimation matrix Ĥ(s) with an accuracy sufficient for some applications such as mobile MIMO-OFDM.
FIG. 14 is a block diagram of an embodiment of a portion 148 of the channel estimator 138 of FIG. 13 corresponding to one transmit antenna and one receive antenna (e.g., receive antenna 132R-1 of FIG. 13) where i is the transmit-antenna index, r is the receive-antenna index, and the channel estimator may determine the partial channel-estimation matrices Ĥr(i,s): (1) recursively without calculating the inverse of a matrix at least in real time, and (2) by accounting for changes in the number, delays, and/or energies of the paths L that compose the communication channels corresponding to the receive antenna. It is contemplated that the portions 148 of the channel estimator 138 corresponding to the other transmit antennas T and to the other receive antennas 132 (if there is more than one receive antenna) may be similar.
The portion 148 of the channel estimator 138 determines the partial channel-estimation matrix Ĥr(i,s) for the communication channel between the ith transmit antenna (e.g., a transmit antenna 116 in FIG. 12) and the rth receive antenna (e.g., a receive antenna 132 in FIG. 13); therefore, for T transmit antennas and R receive antennas, the channel estimator 138 includes R×T portions that may be similar to the portion 148. For example, if R=T=2, then the channel estimator 138 may include 2×2=4 respective portions 148 for the following channels: (i=0, r=0), (i=1, r=0), (i=0, r=1), and (i=1, r=1). An embodiment of a combiner for combining the R×T partial channel-estimation matrices Ĥr(i,s) into a channel-estimation matrix Ĥ(s) is described below in conjunction with FIG. 15.
The partial channel-estimator portion 148 includes a first stage 150 for determining path-independent quantities for the communication channel between the ith transmit antenna and rth receive antenna (hereinafter the (r,i) channel), b parallel second stages 1520-152b-1 for respectively determining column vectors hr,l(i,s) that describe the time-domain responses of the Z paths L of the (r,i) channel during the symbol period s, a communication-path monitor 154 for monitoring the number and delays of the Z channel paths L, and a partial channel-matrix calculator 156 for determining the partial channel-estimation matrix Ĥr(i,s) for the (r,i) channel during the symbol period s.
The first stage 150 determines quantities that are related to the (r,i) channel but that are independent of any particular channel path L, and that may be used by the second and third stages 152 and 156. Examples of, and techniques for determining, such quantities are discussed below. Furthermore, if such a quantity is also independent of either the receive antenna r or the transmit antenna i, then the first stage 150 may provide such quantity to one or more first stages of the other channel-estimator portions 148, or receive such quantity from a first stage of another channel-estimator portion, to reduce or eliminate redundant processing.
Each of the second stages 152 determines a respective time-domain path vector hr,l(i,s) for a respective one of the Z paths L0≦l≦Lz-1. The number b of second stages 152 depends on the path delays that the (r,i) channel may possibly have for a particular application. For example, suppose that even though it is anticipated that the (r,i) channel will not have more than Z=4 simultaneous paths L during a symbol period s, the delays of these paths may range from 0 to 4 samples in increments of 0.25 samples, for a total of 4×1/(0.25)=16 possible path delays. Therefore, in such an example, the partial-channel-estimator portion 148 would include b=16 second stages 1520-15215, one stage for each of the anticipated sixteen path delays, respectively. As discussed below, the path monitor 154 engages the second stages 152 corresponding to the delays of the paths L present in the (r,i) channel.
Each second stage 152 includes a first substage 158, a second substage 160, a third substage 162, and an engage/disengage switch 164.
Each first substage 158 is for determining quantities that are dependent on the particular channel path L of the (r,i) channel associated with the second stage, and that may be used by the corresponding second substage 160. Examples of, and techniques for calculating, such quantities are discussed below. Furthermore, if such a path-dependent quantity is independent of the receive antenna r or transmit antenna i, then the first substage 158 may provide such quantity to one or more first substages of the other channel-estimator portions 148, or receive such quantity from a first substage of another channel-estimator portion, to reduce or eliminate redundant processing.
Each second substage 160 may include a respective recursive filter, such as a Vector State Scalar Observation (VSSO) Kalman filter, which may increase the accuracy of the respective determined vector hr,l(i,s) without increasing the complexity (or even reducing the complexity) of the channel estimator 138 as compared to prior channel estimators. The recursive-filter substage 160 may increase the accuracy of hr,l(i,s) by effectively using information from preceding symbol periods to determine hr,l(i,s) for a current symbol period s. For example, referring to FIG. 12, suppose that the client 114 is moving at an approximately constant velocity relative to the base 112; therefore, from symbol period to symbol period, one would expect the Doppler Spread to be approximately the same. Without the recursive-filter substage 160, the second stage 152 may allow an anomaly, such as a noise “spike,” during a symbol period s to introduce a significant error into the path vector hr,l(i,s), because the second stage has no way to “know” that the Doppler Spread is approximately constant relative to prior symbol periods. But because the recursive-filter substage 160 may track the trend (e.g., approximately constant Doppler Spread) of the response of the path L, it may allow the second stage 152 to lessen, or even eliminate, the error that an anomaly may introduce into hr,l(i,s). Furthermore, one may design the recursive-filter stage 160 such that it does not perform a matrix inversion, at least not in real time; for example, a VSSO Kalman filter does not perform a matrix inversion in real time. This may reduce the complexity of each second stage 152, and thus may reduce the overall complexity of the channel estimator 138 as compared to conventional channel estimators. An embodiment of a recursive-filter substage 160 is described below.
Each third substage 162 determines the respective path vector hr,l(i,s) in response to the second substage 160 as described below.
The communication-path monitor 154 tracks changes to the number, delays, and energies of the communication paths L in the (r,i) channel, and periodically adjusts which of the second stages 152 are engaged and disengaged based on the delays and numbers of paths L that are currently present in the channel. For example, if the path monitor 154 determines that the (r,i) channel currently has Z=4 active paths L having relative delays of 0.0 (the zero-delay path typically is always present), 0.25, 1.25, and 2.0 respectively, then the path monitor engages the second stages 152 corresponding to these delays via the respective switches 164, and disengages the remaining second stages via respective switches 164. The path monitor 154 determines which paths are active (i.e., present for purposes of the receiver 130 of FIG. 13) by monitoring the energies of the paths and comparing the energies to a path threshold. If a path's energy is greater than the threshold, then the corresponding path is active/present; otherwise, the corresponding path is inactive/not present. An embodiment of the path monitor 154 is further described in U.S. patent application Ser. No. 12/963,569, which is incorporated by reference.
The third stage 156 generates the partial channel-estimation matrix Ĥr(i,s) in response to the path vectors hr,l(i,s) from the second stages 152 that the communication-path monitor 154 engages.
An embodiment of the second recursive-filter substage 1600 of the second stage 1520 is now described where the substage 1600 includes a VSSO Kalman filter, it being understood that the second substages 1601-160b-1 may be similar.
The VSSO-Kalman-filter substage 1600 includes an observation scalar calculator 1660, a state-vector predictor 1680, a mean-square-error-matrix predictor 1700, a gain-vector calculator 1720, a state-vector estimator 1740, a mean-square-error-matrix updater 1760, and a scaling-vector calculator 1780; these components are described below.
Before describing the operation of an embodiment of the partial channel-estimator portion 148 of FIG. 14, some MIMO-OFDM channel-estimation-related quantities, and the mathematical relationships between some of these quantities, are described. All of the quantities and relationships described below assume that: (1) APPC pilot clusters Lp (FIG. 8) are used unless otherwise noted (an embodiment of a pilot-symbol pattern that is compatible with the channel estimator 138 (FIG. 13) is discussed below in conjunction with FIG. 17); (2) the pilot clusters Lp in each OFDM signal from a respective transmit antenna are in the same relative positions (i.e., include the same subcarriers); and (3) each of the R×T channels includes the same number Z of paths L.

hr,l(i,s)=[hr,l(i,s)(s), . . . ,hr,l(i,s)(s+N−1)]T  (23)

where hr,l(i,s) is the column vector that represents the time-domain response of the path l of the (r,i) channel during the sth MIMO-OFDM symbol period, s is the first sample time after the cyclic prefix in the sth OFDM symbol (if there is a cyclic prefix), and N is the number of subcarriers k (both pilot and data subcarriers) in the OFDM signal transmitted by the ith transmit antenna. For example, if N=128, s=1 (the symbol period after the 0th symbol period) and the cyclic prefix has four samples, then the OFDM signal transmitted by the ith transmit antenna has a total of 128+4=132 samples, s represents the 268 sample time, and hr,l(i,s) includes one hundred twenty eight complex elements corresponding to the samples 268-395.
In at least some applications, the elements of hr,l(i,s) may be approximated as fitting a curve such as a straight line. Therefore, the elements of hr,l(i,s) may be represented in terms of a polynomial that describes the curve. For example, where the curve is a straight line, which one may represent with the equation y=mx+b where m is the slope of the line and b is the y-axis intercept, hr,l(i,s) may be similarly represented in terms of an offset and slope according to the following equation:

hr,l(i,s)=B hr,l(i,s)  (24)

where B is a binomial expansion matrix having elements (m, n) arranged in Q columns such that B(m,n)=mn (m is the row number and n is the column number), and hr,l(i,s) is a scaling column vector having Q rows/elements; consequently, where the fitting curve is a straight line,





  B
  =
  
    [
    
      
        
          1
        
        
          0
        
      
      
        
          ⋮
        
        
          ⋮
        
      
      
        
          1
        
        
          
            N
            -
            1
          
        
      
    
    ]
  




and hr,l(i,s) is a column vector with Q=2 elements that respectively represent offset and slope. Because typically Q<<N, hr,l(i,s) is typically much smaller (e.g., has many fewer elements), and is thus easier to manipulate, than hr,l(i,s).

The state vector gr,l(i,s) for the engaged filter substage 160 corresponding to the lth path of the (r,i) channel during the symbol period s is given by the following equation:

gr,l(i,s)=[ hr,l(i,s−M+1)T, . . . , hr,l(i,s)T]T  (25)

where M, an integer, is the filter prediction order that provides a filter substage 160 with its recursive feature. For example, to design a filter substage 160 for calculating the state vector gr,l(i,s) using information from the current symbol period and the previous three symbol periods, a designer would set M=4. Generally, the higher the prediction order M, the more accurate the filter substage 160 but the longer its latency, and the lower the value of M, the less accurate the filter substage but the shorter its latency.

The state equation for the engaged filter substage 160 corresponding to the lth path of the (r,i) channel relates the lth path during the current symbol period s to the same lth path during one or more prior symbol periods, and is as follows:

gr,l(i,s)=Agr,l(i,s-1)+er,l(i,s)  (26)

where A is an autoregressive matrix and e is the prediction-error vector. A is dependent on the Doppler Spread, and, therefore, the first stage 150 may determine values of A ahead of time in a conventional manner and store these values in a lookup table, which the first stage may access based on the velocity of the receiver relative to the transmitter; for example, a receiver such as the receiver 130 (FIG. 13) may determine this velocity using a GPS device. Alternatively, the channel estimator 138 may include a conventional linear-adaptive filter (not shown in FIG. 14) that conventionally looks at the pilot symbols recovered by the receiver for one or more prior symbol periods, predicts the pilot symbols to be recovered for the current symbol period s based on the current velocity of the receiver relative to the transmitter, and predicts the value of the A matrix based on the previously recovered pilot symbols and the predicted pilot symbols.

The prediction-error-correlation matrix Gr,l(i) is given by the following equation:

Gr,l(i)=E{er,l(i,s)er,l(i,s)H}  (27)

Although the vector er,l(i,s) may be unknown, its expectation (the right side of equation (27)), which may be generally described as an average of the change in the variance of er,l(i,s) from symbol period to symbol period, depends on the Doppler Spread, and, therefore, may be conventionally determined ahead of time through simulations or with a closed-form expression. Furthermore, because this expectation is approximated to be the same from symbol period to symbol period, the left side of equation (27) is independent of the symbol period s. Consequently, the first substage 158 may determine values for Gr,l(i) dynamically or ahead of time and/or store these values of Gr,l(i) in a lookup table with respect to Doppler Spread, and may retrieve from the lookup table a value of Gr,l(i) for the current symbol period based on the velocity of the receiver relative to the transmitter during the current symbol period.

A channel-independent Np×1 column vector Ppa, which the first substage 158 may calculate and/or store dynamically or ahead of time, is given by the following equation:

Ppa=[Pb+a,Pb+Psep+a, . . . ,Pb+(Np−1)Psep+a]  (28)

where, as discussed above in conjunction with FIGS. 7-8, Pb is the relative center pilot subcarrier of each pilot cluster Lp (and, therefore, is the center pilot subcarrier of the first pilot cluster Lp), Psep is the pilot-cluster separation, and Np is the number of pilot clusters in an OFDM signal transmitted by each transmit antenna. For example, if a signal has Np=3 pilot clusters of LPN=5 pilot subcarriers each, Pb=2, and Psep=8, then Pp−2=[0, 8, 16], Pp−1=[1, 9, 17], Pp0=[2, 10, 18], Pp+1=[3, 11, 19], and Pp+2=[4, 12, 20].
A transmit-antenna-dependent 1×Lp row vector Pcluster(i,c), which the first substage 158 may store ahead of time, is defined as the cth pilot cluster LP transmitted by the ith transmit antenna. For example, where c=0, then the elements of Pcluster(i,0) include the pilot symbols of the 0th pilot cluster Lp transmitted by the ith transmit antenna. The first substage 158 may generate and/or store the vectors Pcluster(i,c) because the receiver 130 (FIG. 13) “knows” the pilot symbols and pilot-cluster locations ahead of time.
A transmit-antenna-dependent value P(i,k), which the first substage 158 may store ahead of time, is the pilot symbol (e.g., in the frequency domain) transmitted from the ith antenna on the kth subcarrier.
A transmit-antenna-dependent pilot-pattern matrix Ppat(i) of dimensions Np×LPN, which the first substage 158 may determine and/or store ahead of time, is given by the following equation:




  
    
      
        
          P
          pat
          
            (
            i
            )
          
        
        =
        
          [
          
            
              
                
                  P
                  cluster
                  
                    (
                    
                      i
                      ,
                      0
                    
                    )
                  
                
              
            
            
              
                ⋮
              
            
            
              
                
                  P
                  cluster
                  
                    (
                    
                      i
                      ,
                      
                        
                          N
                          p
                        
                        -
                        1
                      
                    
                    )
                  
                
              
            
          
          ]
        
      
    
    
      
        (
        29
        )
      
    
  




where, the first row of Ppat(i) includes the pilot symbols that compose the 0th pilot cluster Lp transmitted from the ith transmit antenna, the second row of Ppat(i) includes the pilot symbols that compose the 1st pilot cluster Lp transmitted from the ith transmit antenna, and the (Np−1)th row of Ppat(i) includes the pilot symbols that compose the (Np−1)th pilot cluster Lp transmitted from the ith transmit antenna. In an embodiment, the rows of Ppat(i) may be shifted up or down as long as they remain in a sequence 0-Np−1 and the same shift is applied to all of the matrices Ppat(i) for 0≦i≦T−1 (where T is the number of transmit antennas).

A channel-independent matrix Q (not to be confused with the value Q described above) having the same dimensions Np×LPN as Ppat(i) and which may be stored by the first substage 158 ahead of time, is given by the following equation:




  
    
      
        Q
        =
        
          [
          
            
              
                
                  
                    P
                    b
                  
                  -
                  
                    w
                    p
                  
                
              
              
                ...
              
              
                
                  
                    P
                    b
                  
                  +
                  
                    w
                    p
                  
                
              
            
            
              
                
                  
                
              
              
                ⋮
              
              
                
                  
                
              
            
            
              
                
                  
                    P
                    b
                  
                  +
                  
                    
                      P
                      sep
                    
                    ⁡
                    
                      (
                      
                        
                          N
                          p
                        
                        -
                        1
                      
                      )
                    
                  
                  -
                  
                    w
                    p
                  
                
              
              
                ...
              
              
                
                  
                    P
                    b
                  
                  +
                  
                    
                      P
                      sep
                    
                    ⁡
                    
                      (
                      
                        
                          N
                          p
                        
                        -
                        1
                      
                      )
                    
                  
                  +
                  
                    w
                    p
                  
                
              
            
          
          ]
        
      
    
    
      
        (
        30
        )
      
    
  




That is, the matrix Q includes the subcarrier indices k for the pilot symbols in Ppat(i). For example, if a transmitted signal has Np=3 pilot clusters of LPN=5 pilot subcarriers each, Pb=2, and Psep=8, then Q would equal





  
    [
    
      
        
          0
        
        
          1
        
        
          2
        
        
          3
        
        
          4
        
      
      
        
          8
        
        
          9
        
        
          10
        
        
          11
        
        
          12
        
      
      
        
          16
        
        
          17
        
        
          18
        
        
          19
        
        
          20
        
      
    
    ]
  
  .




A channel-independent (assuming all pilot clusters are in the same relative positions in all i transmitted OFDM signals) column vector PQ having dimensions NpLPN×1 and which the first substage 158 may determine and/or store ahead of time, is given by the following equation:

PQ=[kPb−Wp . . . kPb+Psep(Np−1)+Wp]T  (31)

That is, PQ includes the subcarrier indices k of all pilot subcarriers in an OFDM symbol; or, viewed another way, PQ includes the rows of the matrix Q transposed and “stacked” end to end.

A transmit-antenna- and path-dependent 2Np×LPN matrix θl(i), which the first substage 158 may determine and/or store ahead of time, is given by the following equation:




  
    
      
        
          
            θ
            _
          
          l
          
            (
            i
            )
          
        
        =
        
          [
          
            
              
                
                  e
                  
                    
                      -
                      j2π
                    
                    ⁢
                    
                      
                    
                    ⁢
                    Q
                    ⁢
                    
                      
                    
                    ⁢
                    Δ
                    ⁢
                    
                      
                    
                    ⁢
                    fl
                  
                
              
              
                ⊙
              
              
                
                  p
                  pat
                  
                    (
                    i
                    )
                  
                
              
            
            
              
                
                  e
                  
                    
                      -
                      j
                    
                    ⁢
                    
                      
                    
                    ⁢
                    2
                    ⁢
                    π
                    ⁢
                    
                      
                    
                    ⁢
                    Q
                    ⁢
                    
                      
                    
                    ⁢
                    Δ
                    ⁢
                    
                      
                    
                    ⁢
                    fl
                  
                
              
              
                ⊙
              
              
                
                  p
                  pat
                  
                    (
                    i
                    )
                  
                
              
            
          
          ]
        
      
    
    
      
        (
        32
        )
      
    
  




where





  
    Δ
    ⁢
    
      
    
    ⁢
    f
  
  =
  
    1
    N
  




and the “⊙” operator indicates that each e term is formed using a respective element of the matrix Q, each formed e term is multiplied by a corresponding element of the matrix ppat(i), and this procedure is repeated for all Np×LPN elements of Q and ppat(i), resulting in another Np×LPN matrix. Then, this resulting matrix is effectively “stacked” on itself to obtain the 2Np×LPN matrix θl(i).

Np transmit-antenna- and path-dependent Np×LPN matrices Rl(i,u), which the first substage 158 may determine and/or store ahead of time, are given by the following equation for 0≦u≦Np−1:

Rl(i,u)=θl(i)(u→u+Np−1,:)

where “u→u+Np−1” are the rows of θl(i) used to populate Rl(i,u) and “:” indicates that all columns of these rows of θl(i) are used to populate Rl(i,u).

A transmit-antenna- and path-dependent Np×NpLPN matrix θl(i) (note there is no underline beneath “θ”, this lack of an underline distinguishing this matrix from the matrix θl(i) of equation (32)), which the first substage 158 may determine and/or store ahead of time, is given by the following equation:

θl(i)=[Rl(i,0)Rl(i,1) . . . Rl(i,Np-1)]  (34)

j channel-independent NpLPN×N matrices W(j), which the first stage 150 may calculate and/or store dynamically or ahead of time, is given by the following equation for −Bp≦j≦+Bp:




  
    
      
        
          W
          
            (
            j
            )
          
        
        =
        
          [
          
            
              
                
                  
                    F
                    H
                  
                  ⁡
                  
                    (
                    
                      
                        〈
                        
                          N
                          +
                          
                            (
                            
                              
                                
                                  P
                                  Q
                                
                                ⁡
                                
                                  (
                                  0
                                  )
                                
                              
                              -
                              
                                P
                                b
                              
                              -
                              j
                            
                            )
                          
                        
                        〉
                      
                      ,
                      
                        :
                      
                    
                    )
                  
                
              
            
            
              
                
                  
                    F
                    H
                  
                  ⁡
                  
                    (
                    
                      
                        〈
                        
                          N
                          +
                          
                            (
                            
                              
                                
                                  P
                                  Q
                                
                                ⁡
                                
                                  (
                                  1
                                  )
                                
                              
                              -
                              
                                P
                                b
                              
                              -
                              j
                            
                            )
                          
                        
                        〉
                      
                      ,
                      
                        :
                      
                    
                    )
                  
                
              
            
            
              
                ⋮
              
            
            
              
                
                  
                    F
                    H
                  
                  ⁡
                  
                    (
                    
                      
                        〈
                        
                          N
                          +
                          
                            (
                            
                              
                                
                                  P
                                  Q
                                
                                ⁡
                                
                                  (
                                  
                                    
                                      
                                        N
                                        P
                                      
                                      ⁢
                                      
                                        L
                                        PN
                                      
                                    
                                    -
                                    1
                                  
                                  )
                                
                              
                              -
                              
                                P
                                b
                              
                              -
                              j
                            
                            )
                          
                        
                        〉
                      
                      ,
                      
                        :
                      
                    
                    )
                  
                
              
            
          
          ]
        
      
    
    
      
        (
        35
        )
      
    
  




where F is the known Fourier matrix, the “” operator indicates a modulo N operation, PQ(n) is the nth element of the vector PQ (equation (31)), Pb is the index of the relative center pilot subcarrier of each pilot cluster Lp (and the center pilot subcarrier of the first pilot cluster), and “:” indicates all columns of the matrix FH in the indicated rows. Note that the number of rows in each W(j) matrix is equal to the number NpLPN of pilot subcarriers in each transmitted OFDM signal.

A receive-antenna-dependent column vector yr(s) is given by the following equation for −Bp≦a≦+Bp:

 yr(s)=yr(s)(Ppa)  (36)

where yr(s) is the signal received by the rth receive antenna during the symbol period s, and “(Ppa)” (equation (28)), which for −Bp≦a≦+Bp equals [Pp−Bp . . . PpBp], indicates which elements of yr(s) form yr(s). For example, if there are Np=2 pilot clusters with LPN=5 pilot subcarriers and three (Bp=1) non-guard pilot subcarriers located at subcarriers k=0 (guard), k=1, k=2, k=3, k=4 (guard), and k=8 (guard), k=9, k=10, k=11, k=12 (guard), then for −1≦a≦+1 yr(s) would include the following pilot subcarriers of yr(s) in the listed order: k=1, k=9, k=2, k=10, k=3, k=11.

A transmit-antenna- and path-dependent (but symbol-period-s independent) Np×(2Bp+1) matrix ql(i)H, which the first substage 158 may calculate and/or store dynamically or ahead of time, is given by the following equation:

ql(i)H=[f(iL+l)H . . . f(iL+l)H]  (37)

That is, dl(i)H has 2Bp+1 identical elements, and f(iL+l) is a Np×1 row vector. Examples of f(iL) and f(iL+l) are described below in conjunction with FIG. 17. Using ql(i)H of equation (37) and generating pilot patterns according to the pilot-pattern matrix ppat(i) of equation (54) allow the substages 160 to be VSSO-Kalman-filter substages.

A transmit-antenna- and path-dependent (but symbol-period-s independent) matrix øl(i), which the first substage 158 may determine and/or store ahead of time, is given by the following equation:




  
    
      
        
          ∅
          l
          
            (
            i
            )
          
        
        =
        
          
            [
            
              
                
                  
                    θ
                    l
                    
                      (
                      i
                      )
                    
                  
                
                
                  0
                
                
                  ...
                
                
                  0
                
              
              
                
                  0
                
                
                  
                    θ
                    l
                    
                      (
                      i
                      )
                    
                  
                
                
                  ...
                
                
                  0
                
              
              
                
                  ⋮
                
                
                  ⋮
                
                
                  ⋱
                
                
                  ⋮
                
              
              
                
                  0
                
                
                  0
                
                
                  ...
                
                
                  
                    θ
                    l
                    
                      (
                      i
                      )
                    
                  
                
              
            
            ]
          
          ⁡
          
            [
            
              
                
                  
                    
                      W
                      
                        (
                        
                          -
                          
                            B
                            p
                          
                        
                        )
                      
                    
                    ⁢
                    B
                  
                
              
              
                
                  ⋮
                
              
              
                
                  
                    
                      W
                      
                        (
                        
                          +
                          
                            B
                            p
                          
                        
                        )
                      
                    
                    ⁢
                    B
                  
                
              
            
            ]
          
        
      
    
    
      
        (
        38
        )
      
    
  




A transmit-antenna- and path-dependent (but symbol-period-s independent) row vector ql(i)H (note the bar to distinguish this vector from ql(i)H of equation (37)), which the first substage 158 may determine and/or store ahead of time, is given by the following equation:

 ql(i)H=[01x(M-1)Qql(i)Høl(i)]  (39)

where 01x(M-1)Q is a row vector having (M−1)Q columns/elements that are each equal to zero.

The observation scalar yr,l(i,s) for the engaged filter substage 160 corresponding to the lth path of the (r,i) channel is given by the following equation:

 yr,l(i,s)ql(i)H yr(s)  (40)

The measurement equation for the engaged filter substage 160 corresponding to the lth path of the (r,i) channel is given by the following equation:

 yr,l(i,s)= ql(i)Hgr,l(i,s)+ nr,l(i,s)  (41)

where nr,l(i,s) is the noise due to, e.g., interference on the pilot subcarriers of the (r,i) channel from the data subcarriers and Additive White Gaussian Noise (AWGN) on this same channel. Although nr,l(i,s) may be unknown ahead of time, the first substage 158 associated with the lth path of the (r,i) channel may compute its expectation/variance σr,l2(i)=E{| nr,l(i,s)|2} dynamically or ahead of time by simulation or as a closed-form expression in a conventional manner.

Referring to equation (40) and as further discussed below, the measurement equation effectively relates the symbol recovered during the symbol period s to the response of the (r,i) channel during s, and, referring to equation (41) and also as further discussed below, the state equation (26), via the state vector gr,l(i,s), effectively modifies the result yr,l(i,s) given by the measurement equation (40) based on the response of the (r,i) channel during one or more prior symbol periods. Furthermore, because yr,l(i,s) is a scalar, as discussed below, the filter substage 160 does not invert a matrix (at least not in real time), which may significantly reduce the overall complexity of the channel estimator 138 as compared to a conventional channel estimator.
Still referring to FIG. 14, the operation of an embodiment of the channel estimator 138 is described in terms of the second stage 1520 of the partial channel-estimator portion 148, it being understood that the operations of the other second stages 152 may be similar. Furthermore, in an embodiment, at least one path L0 having a relative delay of zero is always present in the (r,i) channel, and the second stage 1520 is designed to determine hr,l=0(i,s) for the l=L0=0 path of the (r,i) channel having a relative delay of zero; therefore, in such an embodiment, the path monitor 154 always engages the second stage 1520 for the path l=0 of the (r,i) channel having a relatively delay of zero. Moreover, in the example below, the elements of hr,l(i,s) are fit to a straight line as described above.
First, the path monitor 154 determines the number Z and corresponding delays of the paths L that compose the (r,i) channel, and engages, via the switches 164, the second stages 152 that correspond to these paths. As discussed above, for purposes of the following example, it is assumed that the path monitor 154 has engaged at least the second stage 1520.
Next, the first stage 150 may determine and/or store quantities (at least some of which are described above) that the second stage 1520 may need for its calculations, to the extent that the first stage has not already determined and/or stored these quantities. Furthermore, if some of these quantities (e.g. W(j)) are independent of the transmit and/or receive antenna, then the first stage 150 of this or another channel-estimator portion 148 may determine/store these quantities and provide them to the other first stages to reduce or eliminate redundant processing as discussed above.
Similarly, the first substage 1580 may determine and/or store quantities (at least some of which are described above) that the filter substage 1600 may need for its calculations, to the extent that the first substage has not already determined and/or stored these quantities. Furthermore, if some of these quantities are independent of the transmit and/or receive antenna, then the first substage 1580 of this or another channel-estimation portion 148 may determine/store these quantities and provide them to the other first substages to reduce or eliminate redundant processing as discussed above.
Next, the observation-scalar calculator 1660 determines the observation scalar yr,l(i,s) for l=0 of the (r,i) channel according to equation (40).
Then, the state-vector predictor 1680 determines the predicted state vector r,l(i,s) for l=0 of the (r,i) channel according to the following equation:

r,l(i,s)=Aĝr,l(i,s-1)  (42)

Where s=0 (the initial symbol period), the predictor 1680 also provides an initial value for ĝr,l(i,−1). This initial value may be zero, or it may be the expectation of ĝr,l(i,−1). If the initial value is the latter, then the predictor 1680 may compute the expectation of ĝr,l(i,−1) dynamically or ahead of time and store the computed expectation. A technique for calculating the expectation of ĝr,l(i,−1) is described in S. M. Kay, “Fundamentals of Statistical Signal Processing: Estimation Theory,” Prentice Hall: New Jersey (1993), which is incorporated by reference. After the initial symbol period s=0, the state-vector estimator 1740 provides ĝr,l(i,s), which becomes ĝr,l(i,s-1) for the next symbol period s, as discussed below.

Next, the mean-square-error-matrix predictor 1700 determines the predicted mean-square-error matrix r,l(i,s) for l=0 of the (r,i) path according to the following equation:

r,l(i,s)=A{circumflex over (θ)}r,l(i,s-1)AH+Gr,l(i)  (43)

Where s=0 (the initial symbol period), the predictor 1700 also provides an initial value for θr,l(i,−1). This initial value may be zero, or it may be the expectation of the error variance in the state equation (26). If the initial value is the latter, then the predictor 1700 may compute the expectation of the error variance in the state equation dynamically or ahead of time and store the computed expectation. A technique for calculating the expectation of the error variance in the state equation (26) is described in S. M. Kay, “Fundamentals of Statistical Signal Processing: Estimation Theory,” Prentice Hall: New Jersey (1993), which is incorporated by reference. After the initial symbol period s=0, the mean-square-error-matrix updater 1760 provides {circumflex over (θ)}r,l(i,s), which becomes θr,l(i,s-1) for the next symbol period s, as discussed below.

Then, the gain-vector calculator 1720 determines a gain vector Ωr,l(i,s) for l=0 of the (r,i) channel according to the following equation:




  
    
      
        
          Ω
          
            r
            ,
            l
          
          
            (
            
              i
              ,
              s
            
            )
          
        
        =
        
          
            
              
                θ
                 ̆
              
              
                r
                ,
                l
              
              
                (
                
                  i
                  ,
                  s
                
                )
              
            
            ⁢
            
              
                q
                _
              
              l
              
                (
                i
                )
              
            
          
          
            
              
                σ
                _
              
              
                r
                ,
                l
              
              
                2
                ⁢
                
                  (
                  
                    i
                    ,
                  
                  )
                
              
            
            +
            
              
                
                  q
                  _
                
                l
                
                  
                    (
                    i
                    )
                  
                  ⁢
                  H
                
              
              ⁢
              
                
                  θ
                   ̆
                
                
                  r
                  .
                  l
                
                
                  (
                  
                    i
                    ,
                    s
                  
                  )
                
              
              ⁢
              
                
                  q
                  _
                
                l
                
                  (
                  i
                  )
                
              
            
          
        
      
    
    
      
        (
        44
        )
      
    
  




Next, the state-vector estimator 1740 generates the estimated state vector ĝr,l(i,s) for l=0 of the (r,i) channel according to the following equation:

ĝr,l(i,s)=r,l(i,s)+Ωr,l(i,s)[ yr,l(i,s)− ql(i)Hr,l(i,s)]  (45)

As discussed above, ĝr,l(i,s) is fed back to the state-vector predictor 1680 to be used in equation (42) as ĝr,l(i,s-1) for the next symbol period.

Then, the mean-square-error-matrix updater 1760 generates an updated mean-square-error matrix {circumflex over (θ)}r,l(i,s) for l=0 of the (r,i) channel according to the following equation:

{circumflex over (θ)}r,l(i,s)=[IMQ−Ωr,l(i,s) ql(i)H]r,l(i,s)  (46)

where IMQ is an identity matrix of dimensions M(row)×Q(column) and “−” is a minus sign. Furthermore, as discussed above, {circumflex over (θ)}r,l(i,s) is fed back to the mean-square-error-matrix predictor 1700 to be used in equation (43) as {circumflex over (θ)}r,l(i,s-1) for the next symbol period.

Next, the scaling-vector calculator 1780 determines the scaling vector hr,l(i,s) for l=0 of the (r,i) channel for a straight-line approximation of the elements of hr,l(i,s) according to one of the two following equations:

 hr,l(i,s)=ĝr,l(i,s)(MQ−Q:MQ−1)  (47)

 hr,l(i,s-M)=ĝr,l(i,s)(0:Q−1)  (48)

Equation (47) may be referred to as the normal Kalman filter (NKF) output, and equation (48) may be referred to as the Kalman fixed-lag smoother (KFLS) output, which is effectively a low-pass filtered output. Generally, the KFLS output is more accurate, but has a higher latency, than the NKF output.

Then, the third stage path-vector calculator 1620 determines the path vector hr,l(i,s) for l=0 of the (r,i) channel according to equation (24) using either hr,l(i,s) from equation (47) or hr,l(i,s-M) from equation (48).
As stated above, the other engaged second stages 152 of the channel-estimator portion 148 may operate in a similar manner to generate hr,l(i,s) and hr,l(i,s) for the paths l of the (r,i) channel to which they correspond. Typically, all engaged second stages 152 generate hr,l(i,s) according to equation (47) or equation (48) for a symbol period s, although it is contemplated that some second stages may generate hr,l(i,s) according to equation (47) while other second stages may generate hr,l(i,s) according to equation (48) for a same symbol period s.
Next, the third stage partial channel-matrix calculator 156 generates an intermediate partial-channel-estimation matrix Hr(i,s) from the path-response vectors hr,l(i,s) for all of the paths 0≦l≦Z−1 that compose the (r,i) channel according to the following equation:

Ĥr(i,s)(m,n)=ĥr,(m-n)(i,s)(s+m), for 0≦m≦N−1 and 0≦n≦N−1  (49)

Then, the third stage partial-channel-matrix calculator 156 generates the partial-channel-estimation matrix Ĥr(i,s) for the (r,i) channel according to the following equation:




  
    
      
        
          
            H
            ^
          
          r
          
            (
            
              i
              ,
              s
            
            )
          
        
        =
        
          
            1
            N
          
          ⁢
          F
          ⁢
          
            
              
                H
                _
              
              ^
            
            r
            
              (
              
                i
                ,
                s
              
              )
            
          
          ⁢
          
            F
            H
          
        
      
    
    
      
        (
        50
        )
      
    
  




Still referring to FIG. 14, alternate embodiments of the channel estimator 138 and the partial channel-estimator portion 148 are contemplated. For example, alternate embodiments described above in conjunction with the channel estimator 36 of FIGS. 9 and 10 may be applicable to the channel estimator 138. Furthermore, the functions contributed to any of the components of the channel estimator 138 may be performed in hardware, software, or a combination of hardware and software, where the software is executed by a controller such as a processor. Moreover, although described as VSSO Kalman filters, one or more of the second substages 160 may be another type of recursive filter, for example, another type of recursive filter that does not invert a matrix, at least not in real time. In addition, although described as operating in response to APPC pilot clusters (FIG. 9), the channel estimator 138 may be modified (e.g., by modifying some or all of the above equations described in relation to FIGS. 11-14 according to known principles) to operate in response to FDKD pilot clusters (FIG. 8) or other types of pilot clusters. Furthermore, instead of, or in addition to, disengaging the unused second stages 152, the path monitor 154 may cause these unused second stages to enter a low- or no-power mode to save power.
FIG. 15 is a diagram of an embodiment of a partial-channel-estimation-matrices combiner 190 of the channel estimator 138 of FIG. 13.
The combiner 190 generates the RN×TN channel-estimation matrix Ĥ(s) from the RT N×N partial channel-estimation matrices Ĥr(i,s) (for 0≦i≦T−1 and 0≦r≦R−1) according to the following equation:

Ĥ(s)=[(Ĥr=0(i=0,s)Ĥr=0(i=1,s) . . . Ĥr=0(i=T-1,s)); (Ĥr=1(i=0,s)Ĥr=1(i=1,s) . . . Ĥr=1(i=T-1,s)); . . . ;(Ĥr=R−1(i=0,s)Ĥr=R−1(i=1,s) . . . Ĥr=R−1(i=T-1,s))]T  (51)

such that one may think of Ĥ(s) as a matrix that includes R T×N matrices stacked atop one another—note that the matrices within parenthesis (e.g., Ĥr=0(i=0,s)Ĥr=0(i=1,s) . . . Ĥr=0(i=T-1,s) are not multiplied together, but are positioned next to one another.

FIG. 16 is a diagram of an embodiment of a received-signal combiner 136 of the receiver 130 of FIG. 13. The combiner 130 generates the RN×1 received-signal vector y(s) from the R N×1 partial received-signal column vectors yr(s) (0≦r≦R−1) according to the following equation:

y(s)=[yr=0(s)Tyr=1(s)T . . . yr=R−1(s)T]T  (52)

such that one may think of y(s) as a vector that includes 1 column of R N×1 vectors.

FIG. 17 is a diagram of an embodiment of a MIMO-OFDM transmitter 200, which may generate a pilot-symbol pattern ppat(i) (for 0≦i≦T−1) that is compatible with a receiver such as the receiver 130 of FIG. 13.
The transmitter 200 includes T transmit paths 2020-202T-1. For brevity, only the path 2020 is described in detail, it being understood that the remaining paths 2021-202T-1 may be similar.
The transmit path 2020 includes a pilot generator 2040, a data generator 2060, a pilot-subcarrier-coefficient generator 2080, a data-subcarrier-coefficient generator 2100, an Inverse Fourier Transform (IFFT) unit 2120, a digital-to-analog converter (DAC) 2140, a modulator 2160, and an antenna 2180.
The pilot generator 2040 generates pilot subsymbols from pilot information that may include a pilot pattern in the form of a pilot-pattern matrix ppat(i), which is discussed further below.
Similarly, the data generator 2060 generates data subsymbols from data information.
The pilot-subcarrier-coefficient generator 2080 generates from each pilot subsymbol a respective complex frequency-domain coefficient for mapping to the respective pilot subcarrier.
Similarly, the data-subcarrier-coefficient generator 2100 generates from each data subsymbol a respective complex frequency-domain coefficient for mapping to the respective data subcarrier.
The IFFT unit 2120 transforms the pilot-subcarrier and data-subcarrier coefficients into a digital time-domain waveform.
The DAC 2140 converts the digital time-domain waveform into an analog time-domain waveform.
The modulator 2160 modulates a carrier signal (e.g., a 5.4 GHz carrier) with the analog waveform.
And the antenna 2180 transmits the modulated carrier signal for reception by a receiver such as the receiver 130 of FIG. 13. The antenna 2180 may also function as a receive antenna if the transmitter 200 is part of a transmitter/receiver device.
In an embodiment, the pilot generators 204 may each generate a respective pilot pattern according to a respective pilot-pattern matrix ppat(i) such that each column of ppat(i) generated by one of the pilot generators is orthogonal to every column of all the other pilot-pattern matrices ppat(i) generated by the other pilot generators. Such orthogonality is present when the following equation is true:

ppat(m)ppat(n)H=0 for 0≦m≦T−1,0≦n≦T−1, and m≠n  (53)

An example of such orthogonal pilot-pattern matrices is given by the following equation:

ppat(i)=[f(iZ);f(iZ); . . . ;f(iZ)] for 0≦i≦T−1  (54)

where i is the transmit-antenna index, Z is the number of paths L in each channel (in an embodiment it is assumed that each channel always has the same number Z of paths L), and ppat(i) has Np rows (each row represents a pilot cluster) and LPN=2wp+1 identical columns (i.e., f(iZ)f(iZ)H=1).

An example of the Np×1 column vector f(iZ) is given by the following equation:

f(iZ)=[1e−j2πΔfpiZe−j2π2ΔfpiZe−j2π3ΔfpiZ . . . e−j2π(Np−1)ΔfpiZ]  (55)

where





  
    Δ
    ⁢
    
      
    
    ⁢
    
      f
      p
    
  
  =
  
    
      1
      
        N
        p
      
    
    .
  




It has been found that such orthogonal pilot-pattern matrices ppat(i) allow a MIMO-OFDM channel estimator, such as the channel estimator 138 of FIG. 13, to avoid performing a matrix inversion (at least in real time) by including, e.g., recursive filters such as the VSSO Kalman filter substages 160 of FIG. 14.
In another embodiment, the pilot generators 204 may each generate a respective pilot pattern according to a respective pilot-pattern matrix ppat(i) such that not only is each column of ppat(i) generated by one of the pilot generators orthogonal to every column of the pilot-pattern matrices ppat(i) generated by the other pilot generators, but each column of ppat(i) is also orthogonal to every other column of the same matrix ppat(i). Such “dual” orthogonality is present when the following equations are true:

ppat(m)ppat(n)H=0 for 0≦m≦T−1,0≦n≦T−1, and m≠n  (53)

fpat(d)fpat(v)H=0 for 0≦d≦LPN−1,0≦v≦LPN−1, and d≠v  (54)

where fpat(i,u) are the LPN column vectors that compose ppat(i).

An example of such pilot-pattern matrices with dual orthogonality is given by the following equation:

ppat(i)=[f(iLpZ+0Z);f(iLpZ+1Z);f(iLpZ+2Z); . . . ;f(iLpZ+(Lp-1)Z)] for 0≦i≦T−1  (55)

where i is the transmit-antenna index, Z is the number of paths L in each channel (in an embodiment it is assumed that each channel always has the same number Z of paths L), and ppat(i) has Np rows (each row represents a pilot cluster) and LPN=2wp+1 orthogonal columns such that f(iLpZ+d)f(iLpZ+v)H=0 for 0≦d≦(LPN−1)Z, 0≦v≦(LPN−1)Z, and d≠v.

An example of the Np×1 column vectors f(iLpZ+u) for 0≦u≦(Lp−1)Z is given by the following equation:

f(iLpZ+u)=[1e−j2πΔfp(iLpZ+u)e−j2π2Δfp(iLpZ+u)e−j2π3Δfp(iLpZ+u) . . . e−j2π(Np-1)Δfp(iLpZ+u)]  (56)

where





  
    Δ
    ⁢
    
      
    
    ⁢
    
      f
      p
    
  
  =
  
    
      1
      
        N
        p
      
    
    .
  




It has been found that such dual-orthogonal pilot-pattern matrices ppat(i) may improve the performance of a MIMO-OFDM channel estimator that does not include recursive filters such as the VSSO Kalman filter substages 160 of FIG. 14. Furthermore, such dual-orthogonal pilot-pattern matrices ppat(i) may also be usable with a MIMO-OFDM channel estimator, such as the channel estimator 138 of FIG. 13, that includes recursive filters such as the VSSO Kalman filter substages 160 of FIG. 14.
Still referring to FIG. 17, alternate embodiments of the transmitter 200 are contemplated. For example, the modulators 216 may be omitted. Furthermore, the functions performed any of the components of the transmitter 200 may be performed in hardware, software, or a combination of hardware and software, where the software is executed by a controller such as a processor. Moreover, pilot patterns and pilot-pattern matrices other than those described are contemplated.
From the foregoing it will be appreciated that, although specific embodiments have been described herein for purposes of illustration, various modifications may be made without deviating from the spirit and scope of the disclosure. Furthermore, where an alternative is disclosed for a particular embodiment, this alternative may also apply to other embodiments even if not specifically stated. Moreover, the components described above may be disposed on a single or multiple IC dies to form one or more ICs, these one or more ICs may be coupled to one or more other ICs to form a device such as a transceiver, and one or more of such devices may be coupled or otherwise used together to form a system.

## Claims

1. An electronic device comprising:
a plurality of transmit paths each comprising:
a pilot generator configured to receive pilot information and generate pilot sub-symbols based upon the pilot information, the pilot sub-symbols being in a form of a pilot pattern matrix having a dual orthogonality such that
each column of the pilot pattern matrix is orthogonal to each column of a pilot pattern matrix generated by pilot generators in each other transmit path, and
each column of the pilot pattern matrix is orthogonal to each other column of the pilot pattern matrix in a given one of the plurality of transmit paths,

a pilot-subcarrier-coefficient generator coupled to said pilot generator and configured to generate from each pilot sub-symbol a respective complex frequency-domain coefficient for mapping to a respective pilot subcarrier,
a data generator configured to receive data information and generate data sub-symbols, and
a data-subcarrier-coefficient generator coupled to said data generator and configured to generate, from each data symbol, a respective complex frequency domain coefficient for mapping to a respective data subcarrier.

2. The electronic device of claim 1, wherein each of said plurality of transmit paths further comprises an inverse Fourier transform unit circuit coupled to said pilot-subcarrier-coefficient generator and said data-subcarrier-coefficient generator and configured to transform the pilot subcarrier coefficients and data subcarrier coefficients into a digital time-domain waveform.

3. The electronic device of claim 2, wherein each of said plurality of transmit paths further comprises a digital-to-analog converter coupled to said inverse Fourier transform circuit and configured to convert the digital time-domain waveform into an analog time-domain waveform.

4. The electronic device of claim 3, wherein each of said plurality of transmit paths further comprises a modulator coupled to said DAC and configured to modulate a carrier signal with the analog time-domain waveform.

5. The electronic device of claim 4, wherein each of said plurality of transmit paths further comprises an antenna coupled to said modulator.

6. The electronic device of claim 1, wherein said plurality of transmit paths are for a given communication channel; and wherein said electronic device further comprises a further plurality of transmit paths corresponding to a further communications channel.

7. The electronic device of claim 6, wherein a number of said plurality of transmit paths for the given communications channel is equal to a number of said further plurality of transmit paths for the further communications channel.

8. A system comprising:
a transmitter configured to transmit a modulated carrier signal and comprising
a plurality of transmit paths each comprising
a pilot generator configured to receive pilot information and generate pilot sub-symbols based upon the pilot information, the pilot sub-symbols being in a form of a pilot pattern matrix having a dual orthogonality such that
each column of the pilot pattern matrix is orthogonal to each column of a pilot pattern matrix generated by pilot generators in each other transmit path, and
each column of the pilot pattern matrix is orthogonal to each other column of the pilot pattern matrix in a given one of the plurality of transmit paths,

a pilot-subcarrier-coefficient generator coupled to said pilot generator and configured to generate from each pilot sub-symbol a respective complex frequency-domain coefficient for mapping to a respective pilot subcarrier,
a data generator configured to receive data information and generate data sub-symbols, and
a data-subcarrier-coefficient generator coupled to said data generator and configured to generate, from each data symbol, a respective complex frequency domain coefficient for mapping to a respective data subcarrier; and

a receiver operatively coupled to said transmitter and configured to receive the modulated carrier signal.

9. The system of claim 8, wherein each of said plurality of transmit paths further comprises an inverse Fourier transform circuit coupled to said pilot-subcarrier-coefficient generator and said data-subcarrier-coefficient generator and configured to transform the pilot subcarrier coefficients and data subcarrier coefficients into a digital time-domain waveform.

10. The system of claim 9, wherein each of said plurality of transmit paths further comprises a digital-to-analog converter coupled to said inverse Fourier transform circuit and configured to convert the digital time-domain waveform into an analog time-domain waveform.

11. The system of claim 10, wherein each of said plurality of transmit paths further comprises a modulator coupled to said DAC and configured to modulate a carrier signal with the analog time-domain waveform.

12. The system of claim 11, wherein each of said plurality of transmit paths further comprises an antenna coupled to said modulator and configured to transmit the modulated carrier signal for reception by said receiver.

13. The system of claim 9, wherein said plurality of transmit paths are for a given communication channel; and wherein said electronic device further comprises a further plurality of transmit paths corresponding to a further communications channel.

14. The system of claim 13, wherein a number of said plurality of transmit paths for the given communications channel is equal to a number of said further plurality of transmit paths for the further communications channel.

15. A method of communicating using an electronic device comprising a plurality of transmit paths, the method comprising, for each of the plurality of transmit paths:
using a pilot generator to receive pilot information and generate pilot sub-symbols based upon the pilot information, the pilot sub-symbols being in a form of a pilot pattern matrix having a dual orthogonality such that
each column of the pilot pattern matrix is orthogonal to each column of a pilot pattern matrix generated by pilot generators in each other transmit path, and
each column of the pilot pattern matrix is orthogonal to each other column of the pilot pattern matrix in a given one of the plurality of transmit paths;

using a pilot-subcarrier-coefficient generator coupled to the pilot generator to generate from each pilot sub-symbol a respective complex frequency-domain coefficient for mapping to a respective pilot subcarrier;
using a data generator to receive data information and generate data sub-symbols; and
using a data-subcarrier-coefficient generator coupled to the data generator to generate, from each data symbol, a respective complex frequency domain coefficient for mapping to a respective data subcarrier.

16. A non-transitory computer readable medium for an electronic device comprising a plurality of transmit paths, the non-transitory computer readable medium comprising computer-executable instructions to cause the electronic device to perform operations comprising, for each of the plurality of transmit paths:
generating pilot sub-symbols based upon received pilot information, the pilot sub-symbols being in a form of a pilot pattern matrix having a dual orthogonality such that
each column of the pilot pattern matrix is orthogonal to each column of a pilot pattern matrix generated by pilot generators in each other transmit path, and
each column of the pilot pattern matrix is orthogonal to each other column of the pilot pattern matrix in a given one of the plurality of transmit paths;

generating from each pilot sub-symbol a respective complex frequency-domain coefficient for mapping to a respective pilot subcarrier;
generating data sub-symbols; and
generating, from each data symbol, a respective complex frequency domain coefficient for mapping to a respective data subcarrier.