Time series analysis vs DSP terminology

Time series analysis and digital signal processing are closely related. Unfortunately, the two fields use different terms to refer to the same things.

Suppose you have a sequence of inputs x[n] and a sequence of outputs y[n] for integers n.

Moving average / FIR

If each output depends on a linear combination of a finite number of previous inputs

y[n] = b0 x[n] + b1 x[n-1] + … + bq x[nq]

then time series analysis would call this a moving average (MA) model of order q, provided b0 = 1. Note that this might not really be an average, i.e. the b‘s are not necessarily positive and don’t necessarily sum to 1.

Digital signal processing would call this a finite impulse response (FIR) filter of order q.

Autoregressive / IIR

If each output depends on a linear combination of a finite number of previous outputs

y[n] = a1 y[n-1] + … + ap y[np]

then time series analysis would call this an autoregressive (AR) model of order p.

Digital signal processing would call this an infinite impulse response (IIR) filter of order p. 

Sometimes you’ll see the opposite sign convention on the a‘s.


If each output depends on a linear combination of a finite number of previous inputs and outputs

y[n] = b0 x[n] + b1 x[n-1] + … + bq x[nq] + a1 y[n-1] + … + ap y[np]

then time series analysis would call this an autoregressive moving average (ARMA) model of order (pq), i.e. p AR terms and q MA terms.

Digital signal processing would call this an infinite impulse response (IIR) filter with q feedforward coefficients and p feedback coefficients. Also, as above, you may see the opposite sign convention on the a‘s.

ARMA notation

Box and Jenkins use a‘s for input and z‘s for output. We’ll stick with x‘s and y’s to make the comparison to DSP easier.

Using the backward shift operator B that takes a sample at n to the sample at n-1, the ARMA system can be written

φ(B) y[n] = θ(B) x[n]

where φ and θ are polynomials

φ(B) = 1 – φ1B – φ2B² – … φpBp


θ(B) = 1 – θ1B – θ2B² – … θqBq.

System function notation

In DSP, filters are described by their system function, the z-transform of the impulse response. In this notation (as in Oppenheim and Shafer, for example) we have

H(z) = \frac{\sum_{k=0}^q b_k z^{-k}}{1 - \sum_{k=1}^p a_k z^{-k}}

The φk in Box and Jenkins correspond to the ak in Oppenheim and Schafer. The θk correspond to the (negative) bk.

The system function H(z) corresponds to θ(1/z) / φ(1/z).


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Width of mixture PDFs

Suppose you draw samples from two populations, one of which has a wider probability distribution than the other. How does the width of the distribution of the combined sample vary as you change the proportions of the two populations?

The extremes are easy. If you pick only from one population, then the resulting distribution will be exactly as wide as the distribution of that population. But what about in the middle? If you pick from both populations with equal probability, will the width resulting distribution be approximately the average of the widths of the two populations separately?

To make things more specific, we’ll draw from two populations: Cauchy and normal. With probability η we will sample from a Cauchy distribution with scale γ and with probability (1-η) we will sample from a normal distribution with scale σ. The resulting combined distribution is a mixture, known in spectroscopy as a pseudo-Voigt distribution. In that field, the Cauchy distribution is usually called the Lorentz distribution.

(Why”pseudo”? A Voigt random variable is the sum of a Cauchy and a normal random variable. Its PDF is a convolution of a Cauchy and a normal PDF. A pseudo-Voigt random variable is the mixture of a Cauchy and a normal random variable. Its PDF is a convex combination of the PDFs of a Cauchy and a normal PDF. In fact, the convex combination coefficients are η and (1-η) mentioned above. Convex combinations are easier to work with than convolutions, at least in some contexts, and the pseudo-Voigt distribution is a convenient approximation to the Voigt distribution.)

We will measure the width of distributions by full width at half maximum (FWHM). In other words, we’ll measure how far apart the two points are where the distribution takes on half of its maximum value.

It’s not hard to calculate that the FWHM for a Cauchy distribution with scale 2γ and the FWHM for a normal distribution with scale σ is 2 √(2 log 2) σ.

If we have a convex combination of Cauchy and normal distributions, we’d expect the FWHM to be at least roughly the same convex combination of the FWHM of the separate distributions, i.e. we’d expect the FWHM of our mixture to be

2ηγ + 2(1 – η)√(2 log 2)σ.

How close is that guess to being correct? It has to be exactly correct when η is 0 or 1, but how well does it do in the middle? Here are a few experiments fixing γ = 1 and varying σ.

Acoustic roughness examples

Amplitude modulated signals sound rough to the human ear. The perceived roughness increases with modulation frequency, then decreases, and eventually disappears. The point where roughness reaches is maximum depends on the the carrier signal, but for a 1 kHz tone roughness reaches a maximum for modulation at 70 Hz. Roughness also increases as a function of modulation depth.

Amplitude modulation multiplies a carrier signal by

1 + d sin(2π f t)

where d is the modulation depth, f is the modulation frequency, and t is time.

Here are some examples you can listen to. We use a pure 1000 Hz tone and Gaussian white noise as carriers, and vary modulation depth and frequency continuously over 10 seconds. he modulation depth example varies depth from 0 to 1. Modulation frequency varies from 0 to 120 Hz.

First, here’s a pure tone with increasing modulation depth.


Next we vary the modulation frequency.


Now we switch over to Gaussian white noise, first varying depth.


And finally white noise with varying modulation frequency. This one sounds like a prop-driven airplane taking off.


Related: Psychoacoustics consulting

Kalman filters and bottom-up learning

radio antennae

Kalman filtering is a mixture of differential equations and statistics. Kalman filters are commonly used in tracking applications, such as tracking the location of a space probe or tracking the amount of charge left in a cell phone battery. Kalman filters provide a way to synthesize theoretical predictions and actual measurements, accounting for error in both.

Engineers naturally emphasize the differential equations and statisticians naturally emphasize the statistics. Both perspectives are valuable, but in my opinion/experience, the engineering perspective should come first.

From an engineering perspective, a Kalman filtering problem starts as a differential equation. In an ideal world, one would simply solve the differential equation and be done. But the experienced engineer realizes his or her differential equations don’t capture everything. (Unlike the engineer in this post.) Along the road to the equations at hand, there were approximations, terms left out, and various unknown unknowns.

The Kalman filter accounts for some level of uncertainty in the process dynamics and in the measurements taken. This uncertainty is modeled as randomness, but this doesn’t mean that there’s necessarily anything “random” going on. It simply acknowledges that random variables are an effective way of modeling miscellaneous effects that are unknown or too complicated to account for directly. (See Random is as random does.)

The statistical approach to Kalman filtering is to say that it is simply another estimation problem. You start from a probability model and apply Bayes’ theorem. That probability model has a term inside that happens to come from a differential equation in practice, but this is irrelevant to the statistics. The basic Kalman filter is a linear model with normal probability distributions, and this makes a closed-form solution for the posterior possible.

You’d be hard pressed to start from a statistical description of Kalman filtering, such as that given here, and have much appreciation for the motivating dynamics. Vital details have simply been abstracted away. As a client told me once when I tried to understand his problem starting from the top-down, “You’ll never get here from there.”

The statistical perspective is complementary. Some things are clear from the beginning with the statistical formulation that would take a long time to see from the engineering perspective. But while both perspectives are valuable, I believe it’s easier to start on the engineering end and work toward the statistics end rather than the other way around.

History supports this claim. The Kalman filter from the engineering perspective came first and its formulation in terms of Bayesian statistics came later. Except that’s not entirely true.

Rudolf Kálmán published his seminal paper in 1960 and four years later papers started to come out making the connection to Bayesian statistics. But while Kálmán and others were working in the US starting from the engineering end, Ruslan Stratonovich was working in Russia starting from the statistical end. Still, I believe it’s fair to say that most of the development and application of Kalman filters has proceeded from the engineering to the statistics rather than the other way around.

RelatedMore on Kalman filters


Cepstral alanysis vocabulary

An earlier post defined cepstrum and quefrency. This post explains some of the other quirky terms introduced in the same paper by Bogert, Healy, and Tukey. (Given Tukey’s delight in coining words, we can assume he was the member of the trio responsible for the new terms.)

The paper [1] explains why the new twists on familiar words:

In general, we find ourselves operating on the frequency side in ways customary on the time side and vice versa. Experience has made it clear that “words that sound like other words,” although strange at first sight, considerably reduce confusion on balance. These parallel or “paraphrased” words are made by the interchange of consonants or consonant groups, as in “alanysis” from “analysis,” and are introduced as needed.

The magnitude and phase of a cepstrum are called gamnitude and saphe. (The latter explains the pun “saphe cracking” in the title.)

Filtering in the cepstral domain is called liftering. A high-pass filter corresponds to a long-pass lifter and a low-pass filter corresponds to a short-pass lifter.

Harmonics in spectra correspond to rahmonics in cepstra.

Some of these terms are helpful. As explained in the previous post, the independent variable in cepstral analysis, quefrency, differs enough from frequency that it helps to have a separate term for it. Using the terms long and short rather than high and low is helpful for the same reason. Using repiod for the analog of period seems gratuitous, but maybe it’s necessary for consistency. Once you introduce some new terminology, you have to keep going.


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[1] Bruce P. Bogert, M. J. R. Healy, John W. Tukey. The Quefrency Analysis of Time Series for Echoes: Cepstrum, Pseudo-Autocovariance, Cross-Cepstrum and Saphe Cracking. Collected works of John Tukey volume 1

Cepstrum, quefrency, and pitch

John Tukey

John Tukey coined many terms that have passed into common use, such as bit (a shortening of binary digit) and software. Other terms he coined are well known within their niche: boxplot, ANOVA, rootogram, etc. Some of his terms, such as jackknife and vacuum cleaner, were not new words per se but common words he gave a technical meaning to.

Cepstrum is an anagram of spectrum. It involves an unusual use of power spectra, and is roughly analogous to making anagrams of a word. A related term, one we will get to shortly, is quefrency, an anagram of frequency. Some people pronounce the ‘c’ in cepstrum hard (like ‘k’) and some pronounce it soft (like ‘s’).

Let’s go back to an example from my post on guitar distortion. Here’s a note played with a fairly large amount of distortion:


And here is its power spectrum:

single note with distortion

There’s a lot going on in the spectrum, but the peaks are very regularly spaced. As I mentioned in the post on the sound of a leaf blower, this is the fingerprint of a sound with a definite pitch. Spikes in the spectrum alone don’t indicate a definite pitch if they are irregularly spaced.

The peaks are fairly periodic. How to you find periodic patterns in a signal? Fourier transform! But if you simply take the Fourier transform of a Fourier transform, you essentially get the original signal back. The key to the cepstrum is to do something else between the two Fourier transforms.

The cepstrum starts by taking the Fourier transform, then the magnitude, then the logarithm, and then the inverse Fourier transform.

When we take the magnitude, we throw away phase information, which we don’t need in this context. Taking the log of the magnitude is essentially what you do when you compute sound pressure level. Some define the cepstrum using the magnitude of the Fourier transform and some the magnitude squared. Squaring only introduces a multiple of 2 once we take logs, so it doesn’t effect the location of peaks, only their amplitude.

Taking the logarithm compresses the peaks, bringing them all into roughly the same range, making the sequence of peaks roughly periodic.

When we take the inverse Fourier transform, we now have something like a frequency, but inverted. This is what Tukey called quefrency.

Looking at the guitar power spectrum above, we see a sequence of peaks spaced 440 Hz apart. When we take the inverse Fourier transform of this, we’re looking at a sort of frequency of a frequency, what Tukey calls quefrency. The quefrency scale is inverted: sounds with a high frequency fundamental have overtones that are far apart on the frequency domain, so the sequence of the overtone peaks has low frequency.

Here’s the plot of the cepstrum for the guitar sample.

electric guitar cepstrum

There’s a big peak at 109 on the quefrency scale. The audio clip was recorded at 48000 samples per second, so the 109 on the quefrency scale corresponds to a frequency of 48000/109 = 440 Hz. The second peak is at quefrency 215, which corresponds to 48000/215 = 223 Hz. The second peak corresponds to the perceived pitch of the note, A3, and the first peak corresponds to its first harmonic, A4. (Remember the quefrency scale is inverted relative to the frequency scale.)

I cheated a little bit in the plot above. The very highest peaks are at 0. They are so large that they make it hard to see the peaks we’re most interested in. These low quefrency peaks correspond to very high frequency noise, near the edge of the audible spectrum or beyond.

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Electric guitar distortion

Alice Wallace at The Coach House

The other day I asked on Google+ if someone could make an audio clip for me and Dave Jacoby graciously volunteered. I wanted a simple chord on an electric guitar played with varying levels of distortion. Dave describes the process of making the recording as

Fender Telecaster -> EHX LPB clean boost -> Washburn Soloist Distortion (when engaged) -> Fender Frontman 25R amplifier -> iPhone

Let’s look at the Fourier spectrum at four places in the recording: single note and chord, clean and distorted. These are a 0:02, 0:08, 0:39, and 0:43.


Power spectra

The first note, without distortion, has most of it’s spectrum concentrated at 220 Hz, the A below middle C.

spectrum of single note, no distortion


The same note with distortion has a power spectrum that decays much slow, i.e. the sound has more high frequency components.

single note with distortion


Here’s the A major chord without distortion. Note that since the threshold of hearing is around 20 dB, most of the noise components are inaudible.

chord with no distortion


Here’s the same chord with distortion. Notice there’s much more noise in the audible range.

chord with distortion


Update: See the next post an analysis of the loudness and sharpness of the audio samples in this post.

Photo via Brian Roberts CC

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Spectral flatness

White noise has a flat power spectrum. So a reasonable way to measure how close a sound is to being pure noise is to measure how flat its spectrum is.

Spectral flatness is defined as the ratio of the geometric mean to the arithmetic mean of a power spectrum.

The arithmetic mean of a sequence of n items is what you usually think of as a mean or average: add up all the items and divide by n.

The geometric mean of a sequence of n items is the nth root of their product. You could calculate this by taking the arithmetic mean of the logarithms of the items, then taking the exponential of the result. What if some items are negative? Since the power spectrum is the squared absolute value of the FFT, it can’t be negative.

So why should the ratio of the geometric mean to the arithmetic mean measure flatness? And why pure tones have “unflat” power spectra?

If a power spectrum were perfectly flat, i.e. constant, then its arithmetic and geometric means would be equal, so their ratio would be 1. Could the ratio ever be more than 1? No, because the geometric mean is always less than or equal to the arithmetic mean, with equality happening only for constant sequences.

In the continuous realm, the Fourier transform of a sine wave is a pair of delta functions. In the discrete realm, the FFT will be large at two points and small everywhere else. Why should a concentrated function have a small flatness score? If one or two of the components are 1’s and the rest are zeros, the geometric mean is zero. So the ratio of geometric and arithmetic means is zero. If you replace the zero entries with some small ε and take the limit as ε goes to zero, you get 0 flatness as well.

Sometimes flatness is measured on a logarithmic scale, so instead of running from 0 to 1, it would run from -∞ to 0.

Let’s compute the flatness of some examples. We’ll take a mixture of a 440 Hz sine wave and Gaussian white noise with varying proportions, from pure sine wave to pure noise. Here’s what the flatness looks like as a function of the proportions.

spectral flatness

The curve is fairly smooth, though there’s some simulation noise at the right end. This is because we’re working with finite samples.

Here’s what a couple of these signals would sound like. First 30% noise and 70% sine wave:


And now the other way around, 70% noise and 30% sine wave:


Why does the flatness of white noise max out somewhere between 0.5 and 0.6 rather than 1? White noise only has a flat spectrum in expectation. The expected value of the power spectrum at every frequency is the same, but that won’t be true of any particular sample.


How to create Green noise in Python

This is a follow-on to my previous post on green noise. Here we create green noise with Python by passing white noise through a Butterworth filter.

Green noise is in the middle of the audible spectrum (on the Bark scale), just where our hearing is most sensitive, analogous to the green light, the frequency where our eyes are most sensitive. See previous post for details, including an explanation of where the left and right cutoffs below come from.

Here’s the code:

from scipy.io.wavfile import write
from scipy.signal import buttord, butter, filtfilt
from scipy.stats import norm
from numpy import int16

def turn_green(signal, samp_rate):
    # start and stop of green noise range
    left = 1612 # Hz
    right = 2919 # Hz

    nyquist = (samp_rate/2)
    left_pass  = 1.1*left/nyquist
    left_stop  = 0.9*left/nyquist
    right_pass = 0.9*right/nyquist
    right_stop = 1.1*right/nyquist

    (N, Wn) = buttord(wp=[left_pass, right_pass],
                      ws=[left_stop, right_stop],
                      gpass=2, gstop=30, analog=0)
    (b, a) = butter(N, Wn, btype='band', analog=0, output='ba')
    return filtfilt(b, a, signal)

def to_integer(signal):
    # Take samples in [-1, 1] and scale to 16-bit integers,
    # values between -2^15 and 2^15 - 1.
    signal /= max(signal)
    return int16(signal*(2**15 - 1))

N = 48000 # samples per second

white_noise= norm.rvs(0, 1, 3*N) # three seconds of audio
green = turn_green(white_noise, N)
write("green_noise.wav", N, to_integer(green))

And here’s what it sounds like:

(download .wav file)

Let’s look at the spectrum to see whether it looks right. We’ll use one second of the signal so the x-axis coincides with frequency when we plot the FFT.

from scipy.fftpack import fft

one_sec = green[0:N]
plt.xlim((1500, 3000))

Here’s the output, concentrated between 1600 and 3000 Hz as expected:

spectral plot of green noise

Beats: amplitude modulation in radios and musical instruments

What do tuning a guitar and tuning a radio have in common? Both are examples of beats or amplitude modulation.


In an earlier post I wrote about how beats come up in vibrating systems, such as a mass and spring combination or an electric circuit. Here I look at examples from music and radio.


When two musical instruments play nearly the same note, they produce beats. The number of beats per second is the difference in the two frequencies. So if two flutes are playing an A, one playing at 440 Hz and one at 442 Hz, you’ll hear a pitch at 441 Hz that beats two times a second. Here’s a wave file of two pure sine waves at 440 Hz and 442 Hz.

As the players come closer to being in tune, the beats slow down. Sometimes you don’t have two instruments but two strings on the same instrument. Guitarists listen for beats to tell when two strings are playing the same note with the same pitch.

AM radio

The same principle applies to AM radio. A message is transmitted by multiplying a carrier signal by the content you want to broadcast. The beats are the content. As we’ll see below, in some ways the musical example and the AM radio example are opposites. With tuning, we start with two sources and create beats. With AM radio, we start by creating beats, then see that we’ve created two sources, the sidebands of the signal.

Mathematical explanation

Both examples above relate to the following trig identity:

cos(ab) + cos(a+b) = 2 cos a cos b

And because we’re looking at time-varying signals, slip in a factor of 2πt:

cos(2π(ab)t) + cos(2π(a+b)t) = 2 cos 2πat cos 2πbt


In the case of two pure tones, slightly out of tune, let a = 441 and b = 1. Playing an A 440 and an A 442 at the same time results in an A 441, twice as loud, with the amplitude going up and down like cos 2πt, i.e. oscillating two times a second. (Why two times and not just once? One beat for the maximum and and one for the minimum of cos 2πt.)

It may be hard to hear beats because of complications we’ve glossed over. Musical instruments are never perfectly in phase, but more importantly they’re not pure tones. An oboe, for example, has strong components above the fundamental frequency. I used a flute in this example because although its tone is not simply a sine wave, it’s closer to a sine wave than other instruments, especially when playing higher notes. Also, guitarists often compare the harmonics of two strings. These are purer tones and so it’s easier to hear beats between them.


For the case of AM radio, read the equation above from right to left. Let a be the frequency of the carrier wave. For example if you’re broadcasting on AM station 700, this means 700 kHz, so a = 700,000. If this station were broadcasting a pure tone at 440 Hz, b would be 440. This would produce sidebands at 700,440 Hz and 699,560 Hz.

AM signal

In practice, however, the carrier is not multiplied by a signal like cos 2πbt but by 1 + m cos 2πbt where |m| < 1 to avoid over-modulation. Without this extra factor of 1 the signal would be 100% modulated; the envelope of the signal would pinch all the way down to zero. By including the factor of 1 and using a modulation index m less than 1, the signal looks more like the image above, with the envelope not pinching all the way down. (Over-modulation occurs when m > 1. Instead of the envelope pinching to zero, the upper and lower parts of the envelop cross.)

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Related posts:

Creating police siren sounds with frequency modulation

Yesterday I was looking into calculating fluctuation strength and playing around with some examples. Along the way I discovered how to create files that sound like police sirens. These are sounds with high fluctuation strength.

police car lights

The Python code below starts with a carrier wave at fc = 1500 Hz. Not surprisingly, this frequency is near where hearing is most sensitive. Then this signal is modulated with a signal with frequency fm. This frequency determines the frequency of the fluctuations.

The slower example produced by the code below sounds like a police siren. The faster example makes me think more of an ambulance or fire truck. Next time I hear an emergency vehicle I’ll pay more attention.

If you use a larger value of the modulation index β and a smaller value of the modulation frequency fm you can make a sound like someone tuning a radio, which is no coincidence.

Here are the output audio files in .wav format:



from scipy.io.wavfile import write
from numpy import arange, pi, sin, int16

def f(t, f_c, f_m, beta):
    # t    = time
    # f_c  = carrier frequency
    # f_m  = modulation frequency
    # beta = modulation index
    return sin(2*pi*f_c*t - beta*sin(2*f_m*pi*t))

def to_integer(signal):
    # Take samples in [-1, 1] and scale to 16-bit integers,
    # values between -2^15 and 2^15 - 1.
    return int16(signal*(2**15 - 1))

N = 48000 # samples per second
x = arange(3*N) # three seconds of audio

data = f(x/N, 1500, 2, 100)
write("slow.wav", N, to_integer(data))

data = f(x/N, 1500, 8, 100)
write("fast.wav", N, to_integer(data))

Related posts:

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Correlation of two sine waves

What is the correlation of two sine waves that differ in phase? The result itself is interesting, and the calculation along the way shows tricks to avoid calculating integrals.

sines slightly out of phase

The correlation of two periodic signals, f and g, is

\frac{ \int \left( f - \mu_f\right) \left( g - \mu_g\right) \, dt } { \left( \int (f - \mu_f)^2\, dt \right)^{1/2} \left( \int (g - \mu_g)^2\, dt \right)^{1/2} }

where the integral is over a period of the two functions. For functions known at discrete points this would be a sum rather than an integral, but in this case we have continuous signals so we integrate.

In our case the two functions are f(t) = sin(t) and g(t) = sin(t + φ) and the integrals are over [0, 2π]. Both functions have average value 0, so the μ terms go away.

We use a trig identity to expand the numerator:

\sin\theta_1 \sin \theta_2 = \frac{1}{2} \left( \cos(\theta_1-\theta_2) - \cos(\theta_1 + \theta_2) \right)

In our case θ1 = t and θ2 = t + φ and so the numerator becomes

\frac{1}{2} \int_0^{2\pi} \cos\phi - \cos(2t + \phi) \, dt = \pi \cos \phi

The first part of the integral is integrating a constant (with respect to t) and so becomes the constant times the length of the integration range. The second part of the integral is zero because it is integrating a cosine over two periods.

Now for the denominator. Over a full period, sin2(t) and cos2(t) take on the same values, just shifted. So the integral of sin2(t) is half the integral of sin2(t) + cos2(t) = 1. Therefore

\int_0^{2\pi} \sin^2 t\, dt = \frac{1}{2}(2\pi) = \pi

and the same argument shows that the integral of sin2(t + φ) is also π. So our correlation is simply cos φ: the correlation of two out-of-phase sine waves is the cosine of their phase difference. It may be a little surprising that it works out to be so simple, but the result makes sense. When φ = 0, or any multiple of 2π, the waves are identical and so the correlation should be 1. When φ = π, or an odd multiple of π, the two waves are perfectly out of phase, and so the correlation should be -1. In between these extremes the correlation oscillates, in fact it is a cosine.

Energy in frequency modulated signals

In an earlier post we proved that if you modulate a cosine carrier by a sine signal you get a signal whose sideband amplitudes are given by Bessel functions. Specifically:

\cos( 2\pi f_c t + \beta \sin(2\pi f_m t) ) = \sum_{k=-\infty}^\infty J_n(\beta) \cos(2\pi(f_c + nf_m)t)

When β = 0, we have the unmodulated carrier, cos(2π fct), on both sides. When β is positive but small, J0(β) is near 1, and so the frequency component corresponding to the carrier is only slightly diminished. Also, the sideband amplitudes, the values of Jn(β) for n ≠ 0, are small and decay rapidly as |n| increases. As β increases, the amplitude of the carrier component decreases, the sideband amplitudes increase, and the sidebands decay more slowly.

We can be much more precise: the energy in the modulated signal is the same as the energy in the unmodulated signal. As β increases, more enery transfers to the sidebands, but the total energy stays the same. This conservation of energy result applies to more complex signals than just pure sine waves, but it’s easier to demonstrate in the case of a simple signal.


To prove the energy stays constant, we show that the sum of the squares of the coefficients of the cosine components is the same for the modulated and unmodulated signal.The unmodulated signal is just cos(2π fct), and so the only coefficient is 1. That means we have to prove

 \sum_{n=-\infty}^\infty J_n(\beta)^2 = 1

This is a well-known result. For example, it is equation 9.1.76 in Abramowitz and Stegun. We’ll show how to prove it from first principles. We’ll actually prove a more general result, the Newmann-Schläffi addition formula, then show our result follows easily from that.

Newmann-Schläffi addition formula

Whittaker and Watson define the Bessel functions by their generating function:

\exp\left(\frac{z}{2}\left(t - \frac{1}{t}\right)\right) = \sum_{n=-\infty}^\infty t^n J_n(z)

This means that when you expand the expression on the left as a power series in t, whatever is multiplied by tn is Jn(z) by definition. (There are other ways of defining the Bessel functions, but this way leads quickly to what we want to prove.)

We begin by factoring the Bessel generating function applied to zw.

\exp\left(\frac{z+w}{2}\left(t - \frac{1}{t}\right)\right) = \exp\left(\frac{z}{2}\left(t - \frac{1}{t}\right)\right) \exp\left(\frac{w}{2}\left(t - \frac{1}{t}\right)\right)

Next we expand both sides as power series.

\sum_{n=-\infty}^\infty t^n J_n(z+w) = \sum_{j=-\infty}^\infty t^j J_j(z) \sum_{k=-\infty}^\infty t^k J_k(w)

and look at the terms involving tn on both sides. On the left this is Jn(zw). On the right, we multiply two power series. We will get a term containing tn whenever we multiply terms tj and tk where j and k sum to n.

 J_n(z+w) = \sum_{j+k = n} J_j(z) J_k(w) = \sum_{m=-\infty}^\infty J_m(z) J_{n-m} J(w)

The equation above is the Newmann-Schläffi addition formula.

Sum of squared coefficients

To prove that the sum of the squared sideband coefficients is 1,  we apply the addition formula with n = 0, z = β, and w = -β.

1 = J_0(\beta - \beta) = \sum_{m=-\infty}^\infty J_m(\beta) J_{-m}(-\beta) = \sum_{m=-\infty}^\infty J_m(\beta)^2

This proves what we were after:

 \sum_{n=-\infty}^\infty J_n(\beta)^2 = 1

We used a couple facts in the last step that we haven’t discussed. The first was that J0(0) = 1. This follows from the generating function by setting z to 0 and taking the limit as t → 0. The second was that Jm(-β) = Jm(β). You can also see this from the generating function since negating z has the same effect as swapping t and 1/t.

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Quantifying Loudness

How do you quantify how loud a sound is? Sounds like a simple question, but it’s not.

What is loudness?

It’s not hard to measure the physical intensity of a sound, but loudness is the perceived intensity of a sound. It is not a physical phenomena but a psychological phenomena.

Loudness is subjective, but not entirely so. There is general consensus regarding what it means for two sounds to be equally loud, and even for ratios, such as saying when one sound is twice as loud as the other. Loudness is quantifiable, but not easily so.

What does loudness depend on?

Loudness depends on several properties of a sound, such as its frequency, bandwidth, and duration. Loudness must depend on frequency because sounds that are too low or too high have no loudness at all because we simply cannot hear them. But even with the range of audible frequencies, loudness varies quite a bit by pitch. The graph below, via Wikipedia, shows equal loudness contours. The blue lines are from work by Fletcher and Munson in 1937. The red lines are the revised curves per the ISO 226:2003 standard.

Fletcher-Munson curves

The horizontal axis is frequency in Hz and the vertical axis is sound pressure level in decibels. The contour lines represent combinations of frequency and sound pressure level that are perceived to be equally loud. If a tuba and a flute sound equally loud, the sound pressure level coming from the tuba is much higher.

Notice that the curves are not parallel, They’re much closer together for low frequencies than for midrange frequencies, though they are roughly parallel for high frequencies. This means that if you recorded a piano, for example, playing each of its keys at equal loudness, the pitches wouldn’t sound equally loud unless you played the recording back at its original volume.

Complexities and simplifications

As complicated as this is, it’s still a simplification. It is based on pure tones, simple sine waves. A single musical instrument, much less an orchestra or a jackhammer, are more complicated. Loudness is highly nonlinear, and so you cannot say that the loudness of two sounds is the sum of their individual loudnesses. A-weighting is a relatively simple way to convert sound pressure levels to loudness, but is only accurate for pure tones at fairly low loudness levels.

To simplify thing further, consider a single pure tone, a sine wave at 1 kHz. (This is almost two octaves above middle C. See details here.) Loudness level in phons is defined to match sound pressure level in decibels for a 1 kHz pure tone. So a sound has a loudness level of 40 phons, for example, if it is perceived to be as loud as a pure 1 hKz tone at 40 dB.

At 1 kHz, loudness increases by a factor of 2 for every 10 dB increase in sound pressure level. But because nothing is simple in psychoacoustics, even this is a simplification. It only holds for sounds with loudness level 40 dB or greater. A quiet room is around 40 phons, so the added complications below 40 phons may not be relevant in many applications.

A pure tone at 1 kHz and 20 dB sounds more than four times softer than the same tone at 40 dB. The definition of loudness level in phons still holds below 40 phons. An oboe has a loudness level of 20 phons if it has the same loudness as a sine wave with frequency 1 kHz and sound pressure level 20 dB. But an oboe at 30 phons will sound more than twice as loud as one at 20 phons.

Update: New blog post comparing guitar samples at the same sound pressure level but with differing loudness and sharpness.


So where are we as far as calculating loudness? We’ve said a lot about what you can’t do, what complications have to be considered. But we’ve concluded this much: for a pure 1 kHz tone, the loudness in phons equals (by definition) the sound pressure level in decibels. And we’ve said how in principle you could define the loudness of other sounds: compare them to a 1 kHz tone that’s just as loud. We haven’t said how to compute this, only how you could determine it empirically.

In future posts I may write about how you do this using the ISO 532B standard or the newer ANSI S3.4-2007 standard.

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Analyzing an FM signal

Frequency modulation combines a signal with a carrier wave by changing (modulating) the carrier wave’s frequency.

Starting with a cosine carrier wave with frequency fc Hz and adding a signal with amplitude β and frequency fm Hz results in the combination

\cos( 2\pi f_c t + \beta \sin(2\pi f_m t) )

The factor β is known as the modulation index.

We’d like to understand this signal in terms of cosines without any frequency modulation. It turns out the result is a set of cosines weighted by Bessel functions of β.

\cos( 2\pi f_c t + \beta \sin(2\pi f_m t) ) = \sum_{k=-\infty}^\infty J_n(\beta) \cos(2\pi(f_c + nf_m)t)

Component amplitudes

We will prove the equation above, but first we’ll discuss what it means for the amplitudes of the cosine components.

For small values of β, Bessel functions decay quickly, which means the first cosine component will be dominant. For larger values of β, the Bessel function values increase to a maximum then decay like one over the square root of the index. To see this we compare the coefficients for modulation index β = 0.5 and β = 5.0.

First, β = 0.5:

and now for β = 5.0:

For fixed β and large n we have

J_n(\beta) \approx \frac{\beta^n}{2^n \, n!}

and so the sideband amplitudes eventually decay very quickly.

Update: See this post for what the equation above says about energy moving from the carrier to sidebands.


To prove the equation above, we need three basic trig identities

\cos(A + B) &=& \cos A \cos B - \sin A \sin B \\ 2\cos A \cos B &=& \cos(A-B) + \cos(A+B) \\ 2\sin A \sin B &=& \cos(A-B) + \cos(A-B)

and a three Bessel function identities

\cos( z \sin \theta) &=& J_0(z) + 2\sum{k=1}^\infty J_{k}(z) \cos(2k\theta) \\ \sin( z \sin \theta) &=& 2\sum{k=1}^\infty J_{2k+1}(z) \cos((2k+1)\theta) \\ J_{-n}(z) &=& (-1)^n J_n(z)

The Bessel function identities above can be found in Abramowitz and Stegun as equations 9.1.42, 9.1.43, and 9.1.5.

And now the proof. We start with

\cos( 2\pi f_c t + \beta \sin(2\pi f_m t) )

and apply the sum identity for cosines to get

\cos(2\pi f_c t) \cos(\beta \sin(2\pi f_m t)) - \sin(2\pi f_c t) \sin(\beta \sin(2\pi f_m t))

Now let’s take the first term

 \cos(2\pi f_c t) \cos(\beta \sin(2\pi f_m t))

and apply one of our Bessel identities to expand it to

J_0(\beta) \cos(2\pi f_c t) + \sum_{k=1}^\infty J_{2k}(\beta) \left\{ \cos(2\pi (f_c - 2k f_m)t) + \cos(2\pi(f_c + 2k f_m)t) \right\}

which can be simplified to

\sum_{n \,\, \mathrm{even}} J_n(\beta) \cos(2\pi(f_c + nf_m)t)

where the sum runs over all even integers, positive and negative.

Now we do the same with the second half of the cosine sum. We expand

\sin(2\pi f_c t) \sin(\beta \sin(2\pi f_m t))


\sum_{k=1}^\infty J_{2k+1}(\beta) \left\{ \cos(2\pi (f_c - (2k+1) f_m)t) - \cos(2\pi(f_c + (2k+1) f_m)t) \right\}

which simplifies to

\sum_{k=1}^\infty J_{2k+1}(\beta) \left\{ \cos(2\pi (f_c - (2k+1) f_m)t) - \cos(2\pi(f_c + (2k+1) f_m)t) \right\}

where again the sum is over all (odd this time) integers. Combining the two halves gives our result

\cos( 2\pi f_c t + \beta \sin(2\pi f_m t) ) = \sum_{k=-\infty}^\infty J_n(\beta) \cos(2\pi(f_c + nf_m)t)

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