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Photons, Doppler Shift, and Aberration

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A photon has no rest frame, but every massive observer can measure its frequency and direction. Both come from decomposing a nonzero future-directed null four-momentum kμk^\mu relative to the observer’s four-velocity uμu^\mu.

We use kμkμ=0k^\mu k_\mu=0 and absorb ℏ=1\hbar=1, so angular frequency and photon energy have the same numerical value.

Required background. Events, Intervals, and Minkowski Geometry begins the Special Relativity sequence and supplies null geometry; Four-Vectors and Lorentz-Invariant Decomposition supplies four-vector algebra; Observers, Rest Spaces, and Measured Components supplies the observer projector. Helpful background. Calculus and Linear Algebra supplies contractions and projections; Classical and Variational Mechanics supplies relative-velocity and classical wave language.

Frequency and direction as observer measurements

Section titled “Frequency and direction as observer measurements”

The observed frequency is

ω(u)=−kμuμ>0.\omega_{(u)}=-k_\mu u^\mu\gt0.

With

hμν(u)=δμν+uμuν,h^\mu{}_{\nu}(u)=\delta^\mu{}_{\nu}+u^\mu u_\nu,

projecting into the rest space gives

kμ=ω(u)(uμ+n(u)μ),n(u)μ=hμνkνω(u).k^\mu=\omega_{(u)}(u^\mu+n^\mu_{(u)}), \qquad n^\mu_{(u)} =\frac{h^\mu{}_\nu k^\nu}{\omega_{(u)}}.

The null condition implies

uμn(u)μ=0,n(u)μnμ(u)=1.u_\mu n^\mu_{(u)}=0, \qquad n^\mu_{(u)}n^{(u)}_\mu=1.

Thus n(u)μn^\mu_{(u)} is the unit spatial propagation direction measured by uμu^\mu. A telescope’s line of sight to the source points oppositely to the arriving photon’s propagation direction, so observational angle conventions must say which vector is used.

If a source observer usμu_{\rm s}^\mu emits a ray and a receiving observer urμu_{\rm r}^\mu detects the same geometric-optics ray, then

ωrωs=−krμurμ−ksμusμ.\frac{\omega_{\rm r}}{\omega_{\rm s}} =\frac{-k_{{\rm r}\mu}u_{\rm r}^\mu} {-k_{{\rm s}\mu}u_{\rm s}^\mu}.

Here ksk_{\rm s} and krk_{\rm r} are the wave covectors at the two endpoints of one consistently normalized ray. The formula is coordinate independent. In flat spacetime, an inertial ray has constant components in one global inertial chart. As a preview beyond this chapter’s flat-spacetime scope, vacuum geometric optics in curved spacetime parallel-transports kk along the ray, while its coordinate components and its contraction with different observers may change.

In an inertial frame SS, let the photon propagate at angle θ\theta to the positive xx-axis:

kμ=ω(1,cos⁡θ,sin⁡θ,0).k^\mu=\omega(1,\cos\theta,\sin\theta,0).

Let S′S' be the rest frame of an observer moving with velocity +βx^+\beta\hat{\mathbf x} in SS. With the passive boost convention

k′0=γ(k0−βkx),k′x=γ(kx−βk0),k'^0=\gamma(k^0-\beta k^x), \qquad k'^x=\gamma(k^x-\beta k^0),

that receiver has urμ=γ(1,β,0,0)u_{\rm r}^\mu=\gamma(1,\beta,0,0) in SS (and (1,0,0,0)(1,0,0,0) in S′S'), so

ω′=−k⋅ur=γω(1−βcos⁡θ).\omega'=-k\cdot u_{\rm r} =\gamma\omega(1-\beta\cos\theta).

For longitudinal recession, take the source to be at rest in SS, the photon to propagate along +x+x, and the receiver to move along +x+x away from the source. Then cos⁡θ=1\cos\theta=1 and

ω′ω=γ(1−β)=1−β1+β.\frac{\omega'}{\omega} =\gamma(1-\beta) =\sqrt{\frac{1-\beta}{1+\beta}}.

The low-speed limit is 1−β+O(β2)1-\beta+O(\beta^2).

For the approaching arrangement with the same positive receiver velocity, place the stationary source ahead of the receiver. Its photons now travel toward −x-x, so θ=π\theta=\pi and

ω′ω=γ(1+β)=1+β1−β.\frac{\omega'}{\omega} =\gamma(1+\beta) =\sqrt{\frac{1+\beta}{1-\beta}}.

Alternatively, keep the original source behind and reverse the receiver velocity: use β↦−β\beta\mapsto-\beta while keeping θ=0\theta=0. Changing the sign of the velocity and changing the photon direction are two ways to describe approach; neither should be done silently.

Boosting the spatial momentum along xx and dividing by the transformed frequency gives

cos⁡θ′=cos⁡θ−β1−βcos⁡θ,sin⁡θ′=sin⁡θγ(1−βcos⁡θ).\cos\theta' =\frac{\cos\theta-\beta}{1-\beta\cos\theta}, \qquad \sin\theta' =\frac{\sin\theta}{\gamma(1-\beta\cos\theta)}.

These relations preserve cos⁡2θ′+sin⁡2θ′=1\cos^2\theta'+\sin^2\theta'=1. They give the directional aberration that underlies relativistic beaming; an intensity-beaming statement additionally needs the solid-angle Jacobian and the transformation of spectral intensity. For an observer boosted along +x+x relative to an angular distribution in SS, apparent source positions concentrate toward +x+x; because θ′\theta' labels photon propagation, the corresponding arriving propagation vectors concentrate toward −x-x. Keeping those opposite directions distinct prevents a sign reversal in aberration statements.

Combining the formulas gives a useful rapidity form for a boost along the ray:

ω′=e−χω,β=tanh⁡χ.\omega'=e^{-\chi}\omega, \qquad \beta=\tanh\chi.

The exponential appears because collinear rapidities add.

Worked example: ninety degrees in one frame

Section titled “Worked example: ninety degrees in one frame”

There are two inequivalent transverse arrangements. First suppose the photon is transverse in SS, so θ=π/2\theta=\pi/2. Then

ω′=γω,cos⁡θ′=−β.\omega'=\gamma\omega, \qquad \cos\theta'=-\beta.

This is a blueshift. By contrast, suppose the photon is transverse in the receiver frame, so θ′=π/2\theta'=\pi/2. The aberration formula then gives cos⁡θ=β\cos\theta=\beta, and hence

ω′ω=γ(1−β2)=1γ.\frac{\omega'}{\omega} =\gamma(1-\beta^2) =\frac{1}{\gamma}.

This is the standard transverse Doppler redshift. Because aberration changes the angle, “transverse in SS” and “transverse in S′S'” are different experimental arrangements. An angle must always be tagged with its observer.

For a plane wave with phase

Φ=kμxμ,\Phi=k_\mu x^\mu,

an observer samples

dΦdτ=kμuμ=−ω(u).\frac{d\Phi}{d\tau}=k_\mu u^\mu=-\omega_{(u)}.

Frequency is therefore the rate at which phase changes along the observer worldline, up to the stated phase-sign convention. This interpretation extends beyond a particle picture and links directly to geometric optics.

  • A null vector cannot be normalized to −1-1, and a photon has no proper time or comoving rest frame.
  • The endpoint contraction always defines the local measured frequency. The single constant-boost formulas above assume inertial motion in one flat chart; accelerated emitters or receivers can use an instantaneous velocity at each endpoint, while the timing and spectrum of an extended signal depend on their histories.
  • A frequency ratio is not automatically caused only by relative velocity. Gravity, cosmological expansion, media, and source dynamics can also change it.
  • Confusing propagation direction with direction toward the source reverses apparent-angle statements.
  • A plane-wave four-vector and its Lorentz transformation are exact in flat vacuum spacetime. Using a single local ray for a varying wave field additionally requires its wavelength to be short compared with the background and envelope variation scales. Outside that regime, wave packets and full field propagation are needed.

The paired plane-wave transformation of frequency and propagation direction was derived in Einstein 1905, §7, printed pp. 910–912. That historical source supports the special-relativistic Doppler and aberration formulas, not the modern observer contraction or the curved-spacetime preview.

Expand the aberration formula through first order in β\beta and show that, for 0<θ<π0\lt\theta\lt\pi,

θ′=θ+βsin⁡θ+O(β2).\theta'=\theta+\beta\sin\theta+O(\beta^2).
Solution

Expanding the cosine formula gives

cos⁡θ′=cos⁡θ−βsin⁡2θ+O(β2).\cos\theta' =\cos\theta-\beta\sin^2\theta+O(\beta^2).

Write θ′=θ+δθ\theta'=\theta+\delta\theta and expand cos⁡(θ+δθ)=cos⁡θ−δθsin⁡θ+O(δθ2)\cos(\theta+\delta\theta)=\cos\theta-\delta\theta\sin\theta+O(\delta\theta^2). Comparing terms gives δθ=βsin⁡θ+O(β2)\delta\theta=\beta\sin\theta+O(\beta^2). The result refers to the propagation direction; the apparent direction toward the source is opposite.

For the boost convention used above, recover both frequency ratios when (a) θ=π/2\theta=\pi/2 and (b) θ′=π/2\theta'=\pi/2. Explain why the signs of the shifts differ.

Solution

For (a), direct substitution gives ω′/ω=γ\omega'/\omega=\gamma, a blueshift. For (b), setting cos⁡θ′=0\cos\theta'=0 in

cos⁡θ′=cos⁡θ−β1−βcos⁡θ\cos\theta'=\frac{\cos\theta-\beta}{1-\beta\cos\theta}

gives cos⁡θ=β\cos\theta=\beta, so ω′/ω=γ(1−β2)=1/γ\omega'/\omega=\gamma(1-\beta^2)=1/\gamma, a redshift. The conditions specify perpendicularity in different observer rest spaces; aberration prevents them from describing the same photon direction.

Continue to Collision Kinematics and Center-of-Momentum Frames to use invariant four-momentum for multiparticle systems.

  • Einstein, Albert. “Zur Elektrodynamik bewegter Körper” [“On the Electrodynamics of Moving Bodies”]. Annalen der Physik, 4th series 17 / overall volume 322, no. 10 (1905): 891–921. DOI.