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Wireless Communication Wireless Propagation Channel. Sharif University of Technology. Fall 2015 Afshin Hemmatyar. Large scale (overall effects due to distance): Path loss (includes average shadowing) Shadowing (due to obstructions)
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Wireless CommunicationWireless Propagation Channel Sharif University of Technology Fall 2015 AfshinHemmatyar
Large scale (overall effects due to distance): • Path loss (includes average shadowing) • Shadowing (due to obstructions) • Small scale (local effects due to reflection/diffraction): • Multipath fading • Signal fades 30-40dB by just moving • tens of centimeters Propagation Characteristics
Maxwell’s equations • Complex and impractical • Free space path loss model • Too simple • Ray tracing models • Requires site-specific information • Empirical Models • Don’t always generalize to other environments • Simplified power falloff models • Main characteristics: good for high-level analysis Path Loss Modeling
Path loss for unobstructed LOS path • (satellites, microwave links): • P.L. = (4πd/λ)2 • Power falls off: • Proportional to d2 (20dB/dec) • Proportional to f2 (f=c/λ) • Usually power measured with respect to • a reference distance d0: • Pr(d) = Pr(d0)(d0/d)2 • Where for example d0 = 1m (indoor) • and about 100m (outdoor) Free Space LOS Model
Three main effects modeled: • 1. Reflection: • Signal reflection from surfaces with sizes >> λ • 2. Diffraction: • Especially important at sharp edges • -> causes waves go behind direct obstacles • 3. Scattering: • Due to reflection with objects smaller than λ • such as rough surfaces, small objects, trees,… • Requires detailed geometry and dielectric • properties of site. • - Similar to Maxwell, but easier math. • Computer packages often used. Ray Tracing Models
Path loss for one LOS path and one reflected bounce • Good approximation for tall towers (over 50m). • Ground bounce approximately cancels LOS path. • above critical distance faster roll off • ∆ = d”-d’ ≈ 2hthr/d (for d >> hr+ ht) • phase shift θ=2π∆/λ ≈ 4πhthr/(λd) • P.L. = (4πd/λ)2/(GtGr(1-ejθ)) ≈ d4/(ht2hr2GtGr) • Power falls off: • for small d is proportional to d2 • for large d is proportional to d4 and independent of λ Two-Ray Reflection Model
Although much weaker than reflection and • multipath, but main contributor when those not • present, especially for receivers behind hills and • mountains. • A good model is the so-called “knife-edge” model • For ν=0 (marginal direct sight, h=0), diffraction loss =6db Diffraction Model
Use experimental data based on the type of • environment: • Natural: Flat areas, hills, rivers, sea, forest • Man-made: Urban areas, suburban • Models extracted from real data for some typical • scenarios. • Can be fine-tuned by adjusting various parameters • for a specific region. • Commonly used in cellular system simulations Empirical Models (1)
Durbin Model • Use topographic data and LOS/diffraction(knife-edge) • models. • Divide area into grids and use interpolation techniques. • Okumura model • Empirically based (site/freq specific) • Awkward (uses graphs) • Hata model • Analytical approximation to Okumura model • Cost 136 Model • Extends Hata model to higher frequency (2 GHz) • Walfish/Bertooni • Cost 136 extension to include diffraction from rooftops. Empirical Models (2)
Completely experimental model (1968) • Based on extensive measurements in Tokyo • area • Frequency range: 150-2000 MHz • Range: 1-100 Km • Ht: 30-1000m • Hr: 1-10m • Propagation media: Urban, suburban, hilly Okumura Model (1)
Power Loss estimation: • Use free space estimate. • Adjust A using urban measurement. • Adjust for ht and hr (ref ht=200m, hr=3m). • Adjust for various propagation areas. • Advantages: • Covers many scenarios. • Relatively reliable: Max. 10-14dB error • Disadvantages: • Only experimental • Lots of curves required • Not very accurate for rural areas Okumura Model (2)
Basically formulates Okumura data into a • programmable formulation (for freq up to 1.5GHz) • Gives three basic formulas for Urban, suburban • and rural areas (1980). • For example, for urban area the model is as follows: • L(dB)=69.55+26.26log(fc)-13.82log(ht)-(hr) • +(44.9-6.55log(ht))log(d) • d: T-R distance (1-20Km) -> not very accurate for • small cells • a(hr): Correction factor for effective antenna height Hata Model
Used when path loss dominated by reflection. • Most important parameter is the path loss • exponent n, determined empirically. • Lav(d) = Lav(d0) + 10nlog(d/d0) (in dB) • d0 : ref distance > near field areas of antenna • For cellular, d0 in Km and • for microcellular, d0 in tens of meter range • n=2 for free space, n=4 for 2-Ray model • In general, n can take values between 2 and 6. Simplified Path Loss Model (1)
Path Loss Exponent for different environments Simplified Path Loss Model (2)
Models attenuation from obstructions. • Random due to random number and type of • obstructions. • Loss in passing through a wall of thickness d is • s(d)=ce-adwhere a is penetration factor of that wall. • If total thickness of walls in an area is dt then: • s(dt)=ce-adt • Since dt can be modeled as Gaussian: • log(s(dt)) = log(c) - adt • which is a log-normal distribution. Shadowing (1)
So, shadowing typically follows a log-normal • distribution and combined path loss and shadowing • can be modeled as: • L(d) = Lav(d) + Xσ (in dB) • = Lav(d0) + 10nlog(d/d0) + Xσ (in dB) • where X is a Gaussian random variable with mean • zero and variance σ which is typically in the range • of 4 to 12. Shadowing (2)
Fit model to measurement data: • Parameters to estimate: Lav(d0), n, and σ • “Best fit” line through dB data • Lav(d0) obtained from measurements at d0. • Exponent is MMSE estimate based on data • Shadowing variance • Variance of data relative to estimated path loss • model (straight line) Shadowing (3)
Path loss: circular cells • For a given radius, can estimate average power can simplified • path loss model. • Then, using shadowing log-normal model can estimate • percentage of power points in cell boundary with power than • some threshold value: • Next step: Estimate percentage of area that has power • greater than the threshold: • Cell Coverage Area (1)
Path loss + shadowing: amoeba cells • Outage probability: Probability of received power to be below • given minimum in an area. • Cell coverage area: Percentage of cell locations at desired power, • which increases as shadowing variance • decreases. • For example, for n=4 and σ=8, • if at boundary 75% of points are over threshold, • then 90% of the area will have received power above threshold. Cell Coverage Area (2)
Highly dependent on materials, partitioning, … • Tables used for loss of various materials • Three main models: • Log-normal: Similar to shadowing in cellular environments • L(d) = Lav(d0) + 10nlog(d/d0) + Xσ (in dB) • 2) Piecewise liner model (Ericsson): • The loss exponent varies by distance and upper/lower bounds are introduced. • 3) Attenuation Factor: • Take into account attenuation of floors and other obstacles between transmitter and receiver: • L(d) = Lav(d0) + 10nSFlog(d/d0) + FAF + ΣPAF (in dB) • (Same Floor n) (Floor Att.) (Partition Att.) Indoor Models
Large scale effects mainly important in • overall design of network: • Cell radius, Tx power, Frequency planning, … • Small scale effects mainly important in • TX/RX design: • Coding, Modulation, Diversity, Equalizer, … Small Scale Effects (1)
In practice, signals arrive at receiver from • multiple paths with different delays and • attenuations. • Combination of these signals with different • phases, results in an effect known as fading. • Fading causes fast changes in received • power, which is not related to overall path • loss effect introduced earlier. Small Scale Effects (2)
Random Number of multipath components, • each with • Random amplitude • Random phase • Random Doppler shift • Random delay • Random components change with time. • Leads to time-varying channel impulse • response. Small Scale Effects (3)
Random change of received power • (fading) • Random change of carrier frequency • (frequency spread) • Random spread of signal in time • (time spread/ISI) Small Scale Effects (4)
Fading: Random change of received power in space • Due to multipath, vector combination of multiple copies of narrowband signal creates a location-varying distribution of power in space. • This causes large changes in signal power in short distances. • For a moving receiver, this means change of received power in time. • Also, for a fixed receiver, this means that the receiver may get stuck inside a deep fade and never get an acceptable signal . • Use of antenna diversity discussed later. • Fading depends on carrier frequency, so the two-dimension distribution of power is also a function of frequency. • Frequency response of channel at each point of space Small Scale Effects (5)
Frequency Spread:Random change of carrier • frequency • Due to motion of receiver or moving objects in the • environment, the frequency of received signal will • also change randomly. • Doppler Effect: fd = v/λ cos(θ) • Doppler effect causes spread of bandwidth of the • received signal (frequency spread). Small Scale Effects (6)
Time Spread:Random spread of signal in time • Due to multipath, delayed versions of signal arrive at the receiver and are combined. • Therefore, the received signal will also be spread in time. • The time spread effect is not noticeable for narrowband signals and largely affects signal with larger bandwidths. • For digital signals, this will result in ISI (Inter-Symbol Interference). • Need for Equalizer Small Scale Effects (7)
Multipath channel characteristics, number of paths and their attenuation and delay, and its relation to BW of transmitted signal, will determine: • Type of fading in frequency domain • Time spread effects (ISI) • Velocity of movement of Tx, Rx, or surrounding objects, will determine: • Rate of change of fading in time domain • Amount of frequency spread Small Scale Effects (8)
The multipath nature of wireless channel causes • channel frequency response to be non-ideal. • Although channel is in general time varying, for a • given time, the channel can be considered • approximately constant and we can plot frequency • response of the channel. • How the channel frequency response looks like, • depends on number and overall delay of paths • coming from different directions. • What is important in terms of channel response is • the relation between changes in channel response • and signal bandwidth. So a channel can be close to • ideal for one signal, but completely non-ideal for • another one with a larger BW. Frequency Response of Channel (1)
Frequency Response of Channel (2) • For a narrowband signal of BW=10KHz the above channel is close to ideal. • For a GSM signal with BW=200KHz, channel is non-ideal. We will have ISI and equalization becomes essential. • The term “Coherence BW” of a channel, BC, gives range of frequencies over which channel changes are small. (for the above channel, BC=40KHz) • So, what is important is the relation between BC and signal BW.
Time variation is wireless channel are due to relative velocity of transmitter (or main obstacles) and the receiver. • This relative motion causes spread of carrier frequency (Doppler Spread) proportional to the velocity. fd=v/λ cos(θ) frequency range: (fc – fd ) … (fc+fd) • for example: v= 1m/s , λ=10cm, θ=0 fd=10Hz • In addition, motion causes change in channel frequency response (fading variation) in time/space. • Coherence time of a channel • (Tc) is the time over which • channel can be considered • almost constant. Time Response of Channel (1)
Baseband time response of channel at t to • impulse at t-τ: • t is time when impulse response is observed. • t-τ is time when impulse put into the channel. • τis how long ago impulse was put into the • channel for the current observation. • So for a general time varying channel, the • amplitudes, delays and phases of paths will • be different if you apply impulses at • different times. Time Response of Channel (2)
Simplified Time Invariant Impulse Response • In practice, the attenuations and delays • change with time, but changes are rather • slow (compared with bit rate of signal), so • the above model is a good approximation. • Question: What is a good statistical model • for φn , an, and τn ? • Answer: Easy one for φn is uniform [0, 2π]. Time Response of Channel (3)
Statistical behavior of an • Even though an denotes the amplitude of signal • arriving at τn, but an itself can still be the sum of • many smaller paths arriving at “almost” the same • time. • In fact the resolution of a channel in separating • different paths depends on its bandwidth, which in • the best case is the same as the transmitted signal • bandwidth (BW). • So delays with resolution (|τk1-τk2|) less than 1/BW • will be combined together and form an. • In other words each main path an will be formed • from many “subpaths” added together: Time Response of Channel (4)
Statistical behavior of an • Since anejφis formed by sum of many random signals, its I and • Q components will be Gaussian, therefore its envelop an will • have a Rayleigh distribution: • where σ2 is the average power • of the signal before • envelop detection. • Obviously, a Rayleigh random variable will have non-zero mean. • Its mean is equal to 1.25σ. • If an strong LOS path is available, the distribution will be • slightly different and given by Rician distribution. • In this case the random multipath will be added to an almost • stationary LOS signal: • where A denotes • the peak amplitude • of the dominant signal • and I0(.) is the Bessel function of first kind and zero order. Time Response of Channel (5)
Rayleigh and Rician Distributions Time Response of Channel (6)
Statistical behavior of an • Note that, path strength gets weaker as we go • further from main path. • Therefore, the paths with longer delays, τn, will have smaller E[an] Relative power density graphs as • functions of delay. • Also, in some scenarios paths arriving at different • time delays might be correlated, so an can be • somehow correlated for such delays. • Measurements also support another distribution • known as Nakagami distribution in some • environments. • Can model both Rician and Rayleigh, also can • model worse than Rayleigh scenarios as well. • Better for closed form BER expressions. Time Response of Channel (6)
Statistical behavior of τn • The individual path delays can be modeled • by Poisson distribution. • In other words, the difference between path • delays is given by exponential distribution. • However, such models do not work very well • for wireless channels that have “memory”. • In practice, general behavior of path delays • is expressed in terms of the so-called overall • “delay spread”. Time Response of Channel (7)
Time Dispersion Parameters • Mean Excess Delay: • RMS delay spread: • where: • Excess delay spread (for X dB signal): • The amount of delay when the signal power falls • below X dB of strongest arriving path. Time Response of Channel (8)
Examples of RMS delay spread Design for GSM is based on excess delays of up to 18us. Time Response of Channel (9)
As we discussed before, delay spread of • channel impulse response in time domain • determines the variations of channel • response in frequency domain. • Coherence BW of channel: Signals with • frequencies apart more than BC are affected • differently by the channel. • We expect the Coherence BW of channel, • BC, be dependent on channel delay spread. • As channel delay spread increases we expect • smaller BC and therefore faster channel • variations in frequency domain. Delay Spread <1> Coherence BW
The value of BC depends on how much correlation • we specify between correlated carriers. • For correlation above 0.5, we will have: BC ≅ 1/(5στ) • For example, for στ = 20µsec , BC ≅ 10KHz • Signal BW >> BC • ≡ • Symbol duration (TS) << Ch. delay spread (στ) • ISI exists and Equalizer needed • (Signal may be faded in some frequencies.) • Signal BW << BC • ≡ • Symbol duration (TS) >> Ch. delay spread (στ ) • No ISI and No equalizer needed , • (But signal may be totally faded.) Delay Spread <2> Coherence BW
So far we have discussed frequency variations of • signal at a given point in space. • The next question is how the channel changes over • time as the mobile moves with speed of v m/sec? • As we discusses before, these time variations are • directly interconnected with space variations of • signal, as the mobile moves through such space • The parameter that we will use for this concept is • the so-called “coherence time” of the channel, TC. • In order to find TC, an approximation for correlation • function of received signal in time, is found. Freq. Spread <1> Coherence Time
Consider following assumptions: • Narrowband signal with frequency fC • Many paths arriving at receiver from a close to • uniform distribution of angles in space • The received signal is given by: • r(t) = rI(t) cos(2πfCt) + rQ(t) sin(2πfCt) • where rI(t) = Σan cos(ϕn(t)) and rQ(t) = Σan sin(ϕn(t)) • and ϕn(t) = 2π[fCτn + fDnτn – fDnt] • rI(t) and rQ(t) will be jointly Gaussian random • processes and since ϕn(t) is unif [- π, π], therefore, • we will have: • E[rI(t)]=E[rQ(t)] = E[rI(t)rQ(t)] = 0 • Our goal is to find autocorrelation of rI(t) and rQ(t): • ArI(t,τ) = E[rI(t)rI(t+τ)] Freq. Spread <2> Coherence Time
By definition: • ArI(t,τ)=E[rI(t)rI(t+τ)] • =ΣE(an2)E[cos(ϕn(t ))cos(ϕn(t +τ))] • Now substituting ϕn(t) = 2π[fCτn + fDnτn – fDnt], • we will have: E[cos(ϕn(t)ϕn(t +τ)] = 0.5E[cos2πfDnτ] • + 0.5E[cos(4πfCτn + 4πfDnτn - 4πfDnt - 2πfDnτ)] • Since fCτn changes rapidly and has uniform • distribution, the second term will be zero and thus: • ArI(t,τ) = 0.5 ΣE(an2)E[cos(2πfDnτ)] • = 0.5 ΣE(an2)Eθn[cos(2πvτcos(θn)/λC] • where we replaced Doppler frequency with • fD = v/λ cos(θ) for angles of arrival θn at receiver. • Similarly, it can be shown that: • ArI(τ) = ArQ(τ) = ArI(t,τ) Freq. Spread <3> Coherence Time
Now in order to simplify the correlation functions we • make an assumption about angles of arrivals: • If angles of arrival of multipath at receiver are • uniformly distributed then: • Eθn[cos(2πvτcos(θn)/λC]=J0(2πvτ/λC)=J0(2πfDτ) • for fD= v/λC where J0 is a Bessel function of 0thorder • Correlation drops below 0.5 around λC/4 in space. • Usually λC/2 is considered the distance at which • signals are uncorrelated. Freq. Spread <4> Coherence Time
Autocorrelation also gives correlation in time: • vTC = λC/2 Tc = 0.5 λC/v = 1/(2fD) • For usual mobile channels: • fD = 100Hz TC = 5mS • For example for GSM: burst period = 0.5mS • therefore, channel almost constant during each • burst. Freq. Spread <5> Coherence Time
Note: The assumption about angles of arrival is valid • for macrocells but not necessarily microcells. • With this assumption: • ArI(τ) = ArQ(τ) = ΩP/2 J0(2πfDτ) • Ar(τ) = ΩP/2 J0(2πfDτ) cos(2πfCτ) • where ΩP = ΣE(an2) • Also, it can be shown that • the correlation of envelope • of received signal r(t) will • be proportional to J02(2πfDτ). • Note: If spatial angles are • not uniform, the above • approximations are not valid. Freq. Spread <6> Coherence Time
Doppler spread can be obtained by taking • Fourier Transform of autocorrelation • functions: Freq. Spread <7> Coherence Time
Doppler effect usually negligible if fD is much • smaller than signal BW: • fD << BW • Doppler PSD also used in implementing channel • variations in computer simulations. • Generate two independent white Gaussian noise • sources with PSD of N0/2, and then pass them • through a LPF with H(f) that satisfies: • SrI(f) = SrQ(f) = N0/2 |H(f)|2 Freq. Spread <8> Coherence Time