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Radar Distance and Observer-Adapted Coordinates

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One observer can assign a time and a distance to a nearby event by emitting a light signal, having it reflected, and recording its return. The resulting radar quantities are operational but only where the two required null connections exist uniquely. Fermi coordinates use spacelike geodesics instead; they are geometrically convenient, not the outcome of the same measurement procedure.

Required background. Observers, Rest Spaces, and Measured Components provides observer projectors and measured decompositions; Pseudo-Riemannian Metrics and Signature provides Lorentzian norms and causal classification; Frames, Coframes, and Anholonomy provides dual frames and local Lorentz freedom.

Helpful background. Events, Intervals, and Minkowski Geometry supplies the flat-spacetime limit; Tensor Fields and Natural Operations clarifies tensors versus their components; Proper Acceleration and Accelerometer Readings gives operational intuition for carried instruments.

Let γ(τ)\gamma(\tau) be an ideal observer clock parametrized by proper time. Suppose an event qq is joined to the worldline by exactly two relevant null geodesic segments: an outgoing signal leaves at γ(τ−)\gamma(\tau_-), is reflected at qq, and returns at γ(τ+)\gamma(\tau_+). Define

T(q)=τ++τ−2,R(q)=τ+−τ−2.T(q)=\frac{\tau_++\tau_-}{2}, \qquad R(q)=\frac{\tau_+-\tau_-}{2}.

With c=1c=1, RR has units of time and length. Restoring cc gives Dradar=c(τ+−τ−)/2D_{\rm radar}=c(\tau_+-\tau_-)/2. The midpoint convention assigns simultaneity by the observer’s own clock, while the half-round-trip time defines distance. Both are scalars once the worldline, clock parametrization, reflected ray pair, and reflection event are fixed.

Angles supplied by a carried tetrad can supplement (T,R)(T,R) to form radar coordinates. Spherical angular coordinates are singular on the worldline, just as ordinary polar coordinates are singular at their origin; locally one may instead use Xı^=Rnı^X^{\hat\imath}=R n^{\hat\imath}. The definitions and their direct operational interpretation are given in Perlick 2008, §§ 1–2, pp. 1–5, preprint PDF.

Radar distance is not the length of a spacelike curve chosen “at the same time.” It is a two-way signaling observable. The construction also idealizes the reflection as localized and instantaneous; a transponder delay must be calibrated and removed before the mathematical RR is inferred.

The diagram makes the midpoint construction explicit for an inertial clock in Minkowski spacetime. Follow the two future-directed light arrows and compare the reflection time with the two readings on the clock’s worldline.

An inertial clock emits a light signal at tau minus and receives it at tau plus after reflection at q. Both arrows point toward increasing time. The reflection lies at midpoint time T and distance R equal to half the elapsed clock time.

Radar assignment in an inertial Minkowski frame: the reflection event qq lies on light rays sent at τ−=T−R\tau_-=T-R and received at τ+=T+R\tau_+=T+R. Their midpoint gives TT and their half-separation gives RR. The dashed horizontal line is the resulting simultaneity assignment, not a signal. Equal spacetime-axis scales; c=1c=1. Curved and accelerated cases need the two null connections separately.

Near any event on a smooth timelike worldline, a sufficiently small convex normal neighborhood supplies unique connecting geodesics. A still smaller tubular region therefore admits one past-directed and one future-directed null connection to the worldline. In that local radar neighborhood, TT and RR are smooth away from the polar degeneracy at R=0R=0, and the T=constantT={\rm constant} surfaces meet the worldline orthogonally.

Global extension is not guaranteed. Radar assignment fails if either signal is absent, as can happen behind an obstacle or beyond an observer horizon. It also becomes multivalued when lensing, caustics, or self-intersections provide more than one outgoing or returning null ray. Even within a region where the ray pair remains unique, a radar-time surface that is spacelike near γ\gamma need not remain spacelike everywhere. Perlick’s precise local proposition and these distinct nonexistence and nonuniqueness failures appear in Perlick 2008, § 2, pp. 3–5, preprint PDF.

The phrase “the radar distance” must therefore name the selected observer and ray pair. Choosing the earliest return, brightest image, or another branch after multiple imaging is an additional convention, not a recovery of the original unique construction.

Choose a nonrotating spatial triad eı^(τ)e_{\hat\imath}(\tau) along γ\gamma. For qq sufficiently close to the worldline, Fermi coordinates seek a unique proper time τF\tau_F and a unique spacelike vector Xı^eı^(τF)X^{\hat\imath}e_{\hat\imath}(\tau_F) such that

q=exp⁡γ(τF)(Xı^eı^(τF)).q=\exp_{\gamma(\tau_F)} \left(X^{\hat\imath}e_{\hat\imath}(\tau_F)\right).

The connecting spacelike geodesic leaves γ\gamma orthogonally, and its initial length is ρ=(δı^ȷ^Xı^Xȷ^)1/2\rho=(\delta_{\hat\imath\hat\jmath}X^{\hat\imath}X^{\hat\jmath})^{1/2}. Unlike RR, neither ρ\rho nor τF\tau_F is obtained by a two-way light exchange. For a geodesic reference worldline and a parallel-transported tetrad, this is the Fermi normal construction analyzed in Manasse and Misner 1963, pp. 735–743. The local exponential-map basis of the construction is reviewed in Reall 2013, § 4.4, pp. 47–48, PDF.

The Fermi chart ends when the normal exponential map ceases to be one-to-one: spacelike normal geodesics may form caustics or self-intersections, or orthogonal hypersurfaces based at different values of τF\tau_F may intersect. Radar coordinates instead depend on uniqueness of both null legs. There is no general reason for the two domains to end at the same boundary. Close to the worldline they share the same local rest-space geometry to first order, but acceleration and curvature produce different higher-order extensions.

For an inertial observer at the spatial origin of Minkowski coordinates, γ(τ)=(τ,0)\gamma(\tau)=(\tau,\mathbf0), an event q=(t,x)q=(t,\mathbf x) with r=∣x∣r=\lvert\mathbf x\rvert has emission and reception times t−rt-r and t+rt+r. Hence T=tT=t and R=rR=r. The Fermi construction gives the same coordinates because the orthogonal spacelike geodesics are straight lines in constant-tt hyperplanes.

This check fixes the factor of one half and confirms that RR has the dimensions of length in units with c=1c=1. It does not establish equality for accelerated motion or curved spacetime. There, the radar values depend on null propagation in both time directions, whereas the Fermi values depend on a spacelike normal exponential map.

In 1+11+1 dimensional Minkowski spacetime, let an inertial observer follow x=0x=0. A reflection event has coordinates (tq,xq)(t_q,x_q) with xq>0x_q>0. Derive its radar coordinates and explain what would go wrong if two different returning null rays reached the observer.

Solution

The outgoing ray satisfies x=t−τ−x=t-\tau_- and reaches qq, so τ−=tq−xq\tau_-=t_q-x_q. The returning ray satisfies x=tq+xq−tx=t_q+x_q-t and reaches x=0x=0 at τ+=tq+xq\tau_+=t_q+x_q. Therefore

T=τ++τ−2=tq,R=τ+−τ−2=xq.T=\frac{\tau_++\tau_-}{2}=t_q, \qquad R=\frac{\tau_+-\tau_-}{2}=x_q.

If two returning null rays arrived at distinct proper times, the same event and outgoing signal would produce two values of τ+\tau_+ and hence two pairs (T,R)(T,R). A branch-selection rule could label them, but the radar assignment would no longer be a single coordinate map.

Now consider an accelerated observer at X=0X=0 in the flat Rindler metric

ds2=−(1+aX)2dT2+dX2,a>0,X>−a−1.ds^2=-(1+aX)^2dT^2+dX^2, \qquad a\gt0,\quad X\gt-a^{-1}.

Its proper time is TT. A reflector remains at X=ρ>0X=\rho\gt0. Find the radar distance to a reflection event and compare it with the Fermi distance ρ\rho on a constant-TT slice.

Solution

For each radial null leg, ∣dT∣=∣dX∣/(1+aX)|dT|=|dX|/(1+aX). Stationarity makes the outward and return coordinate durations equal:

ΔT=∫0ρdX1+aX=ln⁡(1+aρ)a.\Delta T=\int_0^\rho\frac{dX}{1+aX} =\frac{\ln(1+a\rho)}{a}.

If reflection occurs at TqT_q, emission and reception occur at Tq∓ΔTT_q\mp\Delta T. Hence the radar time is TqT_q, but

R=ln⁡(1+aρ)a=ρ−12aρ2+O(a2ρ3).R=\frac{\ln(1+a\rho)}{a} =\rho-\frac12a\rho^2+O(a^2\rho^3).

The constant-TT normal geodesic has length ρ\rho, so the two distances agree to first order near the observer and differ at the next order even though curvature is zero. Taking a→0a\to0 recovers R=ρR=\rho. This makes concrete why a two-way light distance and a spacelike proper length are different constructions.