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Phase Noise Eects on OFDM Wireless LAN Perormance This article quantiies the eects o phase noise on bit-error rate and oers guidelines or noise reduction By John R. Pelliccio, Heinz Bachmann and Bruce W. Myers Raytheon RF Networking onsumers are looking to wireless data transceivers to convey all types o inormation. From 3G cell phones to wireless LANs, the convergence o voice, data and video is driving the demand or wireless gear that is capable o transmitting arther, aster and more eiciently than ever beore. In the wireless LAN industry, or example, the past ew years have seen a migration rom and megabit per second (Mbps) radios to the recent prolieration o Mbps devices. Driven by the insatiable demand or bandwidth, manuacturers are rolling out plans or products capable o data rates as high as 5 Mbps at requencies in the 5 to 6 GHz range. These products, based on industry standards such as the IEEE s 80.(a) and the European Telecom Standards Institute s HiperLAN, use a unique and spectrally eicient modulation scheme known as orthogonal requency division multiplexing (OFDM) to communicate. OFDM is essentially a series o orthogonally separated subcarriers each with its own modulated waveorm. OFDM is very robust against multipath signals and amplitude and group delay variations in the channel. Although this waveorm type is very well suited to an indoor environment, it presents some unique challenges to system designers. The waveorm properties that most aect the analog design are accommodation o an inherently high peak to average power ratio (up to db), sensitivity to non-linearities o the analog components (i.e., gain compression and AM to PM conversion), and sensitivity to phase noise. A system Figure. onstellation diagram o a 6-QAM subcarrier with no distortion. designed without the appropriate amount o margin in any o these categories will generate an unacceptable number o bit errors. An 80.(a) transceiver uses a total o 6 separate subchannels, each spaced 3.5 khz apart, or a total channel bandwidth o 0 MHz. O these subchannels, 8 are used or data, while are unpopulated to allow or guardbands at the channel edges, and our are reserved exclusively or pilot tones. The 8 data subchannels are each modulated independently. Modulations range rom BPSK or 6 Mbps data transer through 6-QAM or 5 Mbps service. A single QAM symbol o modulation level n can 68 APPLIED MIROWAVE & WIRELESS

Figure. onstellation diagram o a 6-QAM subcarrier with distortion. Figure 3. onstellation error vector deinition. carry n bits, so one 6-QAM symbol can convey 6 bits o inormation. The constellation diagram o a 6-QAM subcarrier is shown in Figure. The constellation diagram shows all possible states on the complex plane that a 6-QAM symbol can assume. However, additive white Gaussian noise (AWGN), transmitter and receiver nonlinearities and multipath eects aect QAM symbols. A received QAM symbol may look like the example in Figure. Every QAM receiver has a processor that takes each bit and determines its position in the constellation relative to the origin and a set o predeined decision boundaries. When a symbol crosses a decision boundary, a bit error results. The system must thereore be designed so that this happens inrequently. Since the decision boundaries are placed closer together as the QAM order increases, the requirements placed on the modulated signal become more restrictive as higher order modulations are used. In principle, the error contribution could be allocated between the transmitter and receiver in any proportion. However, 80.(a) speciies that each transmitter must, over the course o a deined number o symbols and packets, provide an average error vector (deined as the distance rom the ideal symbol point to the location in the constellation at which it is actually received) less than a certain magnitude. This magnitude decreases as the data rate (and QAM order) increase, rom 5 db at 6 Mbps to 5 db at 5 Mbps. This constellation error speciication allows interoperability between dierent vendors products by ensuring that neither transmitters nor receivers are designed so that they produce so much error that an interoperable product will not be able to resolve the signals with a good degree o accuracy. Several actors can impact this error vector. AM/AM conversion in the transmit ampliier due to gain compression can cause errors in the intended amplitude o the transmitted symbol. AM/PM conversion and phase noise can cause errors in the phase component o the error vector. There are two important points to note regarding the contributors to constellation error. One is that since the magnitude o the error vector is derived rom a combination o all these actors, reducing the magnitude o one error contributor allows more latitude or the others. For example, i an extremely linear ampliier is used, amplitude distortion will be minor and so AM/PM conversion and phase noise can be allowed to be larger. The second important note is that while AM/AM and AM/PM conversion can be predicted and proactively corrected (or example, through digital predistortion), phase noise is by deinition a random process. Thus, the amount o phase noise in a system will always have a direct and irreversible eect on the quality o the received signal. Every active component in a transmitter and receiver can generate phase noise. However, or practical purposes the requency synthesis components o the system tend to contribute ar more noise than ampliiers and other types o circuits. Everything in the requency synthesizer, rom the reerence requency generator to the phase locked loops to the local oscillators, contributes to the overall phase noise power o the system. I the phase noise power is too high, the resultant error vector in the received constellation will be large, decision boundaries will be crossed, and bit errors will result. Like most parameters in a system design, the amount 70 APPLIED MIROWAVE & WIRELESS

Figure. onstellation diagram o a 6-QAM subcarrier with phase noise. Figure 5. BER or OFDM signal with dierent amounts o phase noise. o allowable phase noise in an OFDM system becomes a question o compromise. omponents with ultra-low phase noise speciications are readily available, but are oten large and expensive. onversely, trying to overintegrate a system to save on parts count or board space can cause problems i the processes or components used do not have phase noise speciications that will lead to an acceptable phase noise power in the inal analysis. How, then, can the eect o phase noise be determined? Phase noise has two eects on an OFDM system. The irst is that it causes a phase shit in the received signal so that its constellation might appear as shown in Figure. The second eect o phase noise is to cause the receiver requency reerence to not align properly with the transmitted signal, causing loss o orthogonality and thereby introducing interchannel intererence (II). These eects are not diicult to alleviate. As discussed earlier, phase noise is mostly due to the synthesizer, with most o the noise power being near the nominal carrier requency. To compensate or dierences in the requency sources o the transmitter and receiver, some tracking o the received signal must be employed. The tracking algorithm will also ollow and thus compensate or any low-requency phase noise. In act, it has been determined that the presence o the requency tracking algorithm allows us to negate the eects o phase noise located closer to the carrier than about 0 percent o the subcarrier spacing. IEEE 80.a requires that the RF requency and data clocks be derived rom the same source. By tracking the carrier requency, it is possible to also compensate or dierences in data clocks at the same time, thus maintaining orthogonality. It is evident, then, that the amount o allowable phase noise in an OFDM system needs to be quantiied so that the requency synthesis section o the OFDM radio is neither overdesigned nor underdesigned. Since the primary system design goal is a low bit error rate, the designer must decide upon an acceptable increase in the carrier to noise ratio (NR) at the operating bit error rate due to phase noise. Figure 5, obtained through simulation, shows the eect o residual phase noise with a ew dierent RMS values on an OFDM signal using 6- QAM subcarriers. Note that the NR required or a speciic bit error rate will decrease depending on the decoding algorithm employed. Figure 5 shows raw results, without the beneit o decoding. The residual phase noise depends upon the implementation o the tracking loop. The ollowing example may serve to illustrate the considerations needed to design the requency sources used in the transceiver. onsider the demodulation scheme illustrated in Figure 6 (note that this is an oversimpliication presented or discussion purposes only). An OFDM signal s(t) with quadrature amplitude-modulated subcarriers is passed to a tracking loop, a second order phase locked loop, with a corner requency. Because is much smaller than the bandwidth o s, the VO output is close to the ideal carrier requency with no modulation. Multiplying this with the modulated signal and removing the high-side mixing product results in recovery o the baseband signal. 7 APPLIED MIROWAVE & WIRELESS

We begin with the power transer unction o the second order PLL in the tracking loop that can be approximated by S Track ( ) + () Figure 6. Demodulator unctional block diagram. Let us urther assume that the source used to generate the carrier has phase noise that ollows the Lorentzian model [], the single-sided noise density spectrum o which is deined by Sd( ) π + () where l is the 3 db linewidth o the oscillator and is the oset rom the carrier requency at which the phase noise density unction S d () is evaluated as depicted in Figure 7. Then the remaining phase noise at the output o the VO would be S VO ( ) π + + (3) Figure 7. Lorentzian phase noise power spectrum with hertz linewidth. For this discussion we will assume that the VO itsel does not generate any noise. Phase noise at requencies that are smaller than the corner requency will then be tracked by the PLL and thereore introduce no errors into the demodulation process. Phase noise outside o the loop bandwidth, however, will cause misalignment o the FFT spacing as well as phase rotations to the recovered symbols and thereore increase the bit error rate. Let us assume that the degradation caused by.5 degrees o phase noise is acceptable. The question is how to design the synthesizer and select the tracking loop bandwidth so that the remaining RMS phase noise not tracked does not exceed.5 degrees. At the baseband output, the noise power density aecting the demodulation would then be the dierence between that o the receiver input and the tracking loop output, or ( ) S π + + and might appear as shown in Figure 8. Figure 8 was generated with a 3 db linewidth o hertz and a tracking loop bandwidth o khz. The remaining phase noise introduces a phase error that ollows a Gaussian distribution. The RMS value or small RMS phase angles ϕ (that is, or ϕ << radian) (standard deviation) can be determined in radians as () 7 APPLIED MIROWAVE & WIRELESS

Figure 8. Phase noise power spectrum density ater demodulator. Figure 9. RMS phase noise versus /. ϕ RMS where B is the channel bandwidth. Evaluation o the integral in Equation (5) is straightorward but quite tedious, and the derivation is not presented here. Although only the power within the channel bandwidth need be considered, the integral is easier to evaluate rom 0 to ininity. This is a legitimate approximation because the loop bandwidth must be much smaller than the carrier bandwidth or this demodulation scheme to work, and power in the bandwidth outside o B will be very small. The so evaluated integral can be written as 0 05. B 0 ( ) Sd ( ) + It ollows that Sd + (5) (6) where ϕ RMS is in radians. Equation (7) shows that the RMS phase noise angle is a unction o the ratio o the receive tracking loop bandwidth to the Lorentzian linewidth, as shown in Figure 9. It remains to select values or receive tracking loop bandwidth and Lorentzian linewidth l. In general, must be narrow enough so that no modulated inormation is lost. In the case o IEEE 80.(a), the subchannel at the center requency is not used and thereore contains no inormation. The edge o the irst occupied subchannel is at 56.5 khz. Let us assume that we want the tracking loop to suppress any modulation at that requency by 30 db. We determine the loop bandwidth by solving (I) or, inserting 56.5 khz or and 0 3 ( 30 db) or S Track, and arrive at a value 7.8 khz as the largest allowable tracking loop bandwidth. From Figure 9 we see that, i the phase noise into the receiver is Lorentzian, the 3 db linewidth must be no greater than 0 3 the tracking bandwidth, or 7.8 Hz. In reality, the models o the carrier phase noise and receive tracking loop are more complex. However, the ollowing basic design rules can be used: ϕ RMS + + (7) Determine an acceptable tracking bandwidth or your application. Design a tracking loop with a response S Track () that provides suicient suppression in the bands o interest. Design a synthesizer with a noise proile S d () so 76 APPLIED MIROWAVE & WIRELESS

Figure 0. Phase noise proiles o requency synthesis components. that the most o the phase noise spectrum alls well within the receiver tracking bandwidth. Determine the RMS phase noise (in radians) at the demodulator output as ϕ RMS 05. B ( Track ) Sd S d ( ) ( ) 0 (8) Determine (perhaps through simulation) whether this phase noise will degrade perormance to an unacceptable level. Equation (8) is valid only i there is no signiicant phase noise contribution rom the receive tracking loop. This should be the case i tracking is implemented as a digital PLL. In implementing the transmit synthesizer, care must be taken to use components that minimize phase noise ar removed rom the carrier. An actual synthesizer constructed o real components tends to have a phase noise spectrum dominated by VO noise rom the edge o the loop ilter bandwidth to the edge o the system noise bandwidth, encompassing requencies ar rom the carrier requency. Reerence requency generators such as crystals generally possess phase noise spectra concentrated close to the carrier. While we have established that this noise will be negated by the tracking loop in the receiver, a low phase noise crystal is important or other system considerations such as meeting the 80.a transmitter constellation accuracy requirements. The crystal requency is generally much lower than the LO requencies, and must be multiplied by n inside the PLL. The crystal phase noise is correspondingly multiplied by 0 log (n) where n is the multiplication actor required to arrive at the output requency rom the reerence requency. Thereore, a better approximation o a phase noise spectrum or an OFDM system would include the crystal phase noise, PLL loop response, and VO phase noise as well as other, less prominent contributors, such as reerence supression ilters, summed together to generate a total SSB phase noise spectrum. A sample o such a summation is presented in Figure 0. are should be taken to speciy components (or analog cells and processes, i synthesizer components are to be integrated into larger unctional blocks) that are capable o meeting the phase noise requirements or a given system BER. onclusion It has been established that phase noise causes an uncancellable and detrimental eect on the accuracy o an OFDM system, measurable as an increase in bit error rate. Simulation results depicting the eect o various levels o phase noise upon the BER o a 6-QAM system have been presented. An example o how to deine the tracking ilter bandwidth necessary to comply with the chosen level o residual phase noise has been presented. Once the tracking ilter bandwidth is deined, some guidelines or designing a real-world synthesizer with a noise spectrum largely within the stated tracking bandwidth are presented and some general design guidelines or choosing real-world components capable o suiting the system phase noise speciications have been established. Reerences. Richard Van Nee and Ramjee Prasad, OFDM or Wireless Multimedia ommunications, New York: Artech House, 000. 78 APPLIED MIROWAVE & WIRELESS

Author inormation John R. Pelliccio is a senior engineer with Raytheon s RF Networking business unit in Marlborough, MA. His primary ocus since joining Raytheon in 995 has been the design, manuacture and implementation o WLAN systems. He has lectured and presented on the emergence o WLAN standards to a variety o industry and educational groups across the United States and abroad. He is the lead RF engineer or Raytheon s recently announced Tondelayo 5 Mbps WLAN chipset. He holds a BSEE degree with distinction rom Worcester Polytechnic Institute. He may be contacted via e-mail at John_R_Pelliccio@raytheon.com. Heinz Bachmann is a senior principal engineer with Raytheon ompany in Marlborough, MA, where he has worked on systems engineering and RF design o commercial wireless products since January 000. His interests include mathematical modeling and computer simulation o communications systems and circuits. Previously, he has worked in satellite communications or Raytheon ompany (996 to 000) or GTE (986 to 993) and in commercial ixed-service point-topoint radio communications or Advanced Techom, Inc. (993 to 996). He received his diploma in electrical engineering rom the Federal Institute o Technology, Zürich, Switzerland in 986. He may be contacted via e-mail at Heinz_ Bachmann@res.raytheon.com Bruce W. Myers has 3 years o experience in engineering and management o communications and radar systems. He is the director o the RF Networking business unit within Raytheon ommercial Electronics. He previously held positions in Raytheon RF omponents including deputy director o engineering and manager o the Wireless Systems Department. He received a BSEE rom Michigan State University in 977 and an MSEE rom Worcester Polytechnic Institute in 983. He is co-author o ive papers and a winner o the IEEE s Wheeler Award and Raytheon s Thomas L. Phillips Award or Excellence in Technology. He may be contacted via e-mail at Bruce_W_Myers@raytheon.com. ircle 39 80 APPLIED MIROWAVE & WIRELESS