Rydberg atom electric field sensors are tunable quantum sensors that can perform sensitive radio frequency measurements. Their qualities have piqued interest at longer wavelengths where their small size compares favorably to impedance-matched antennas. Here, we compare the signal detection sensitivity of cm-scale Rydberg sensors to similarly sized room-temperature electrically small antennas with active and passive receiver backends. We present and analyze effective circuit models for each sensor type, facilitating a fair sensitivity comparison for cm-scale sensors. We calculate that contemporary Rydberg sensor implementations are less sensitive than unmatched antennas with active amplification. However, we find that idealized Rydberg sensors operating with a maximized atom number and at the standard quantum limit may perform well beyond the capabilities of antenna-based sensors at room temperature, the sensitivities of both lying below typical atmospheric background noise.

The radio frequency (RF) spectrum spans more than nine orders of magnitude in frequency, from near-DC to 1012 Hertz. Due to an increasingly crowded spectrum, modern technologies demand more agility and sensitivity over this large, but finite, usable phase space. Recently, RF sensors based on highly excited atomic Rydberg states have achieved sensitivity across the RF spectrum, demonstrating their broad tunability.1–5 Rydberg quantum sensors operate based on the quantum physics of atom–photon interactions and are limited by quantum projection noise instead of internal thermal noise.6–8 Therefore, they do not obey the same limits as traditional antenna-based sensors. In this work, we derive and compare idealized and practical sensitivity limits of Rydberg sensors and antenna-based RF sensors with classical electronic readout.

Here, we focus on signal detection in the electrically small regime, where the system size is much smaller than the carrier wavelength λ. In this limit, matched antenna-based sensors that efficiently absorb the field energy are often impractical or even impossible to build. This is because a lossless and matched antenna must be resonant with a large quality factor Q resulting in low bandwidth ωBW1/Q.9,10 Significant research has been conducted on alternative passive and active antenna-based systems to enable more efficient sensing in the electrically small regime. Examples include active non-Foster circuits,11,12 optimal matching schemes,13,14 and active receiver systems.15 The relationship between Rydberg sensors and antenna-based RF sensors, including active circuits, is an area of ongoing study.2,16,17

In this work, we first derive the RF detection sensitivities of electrically small antennas coupled to optimal active and passive electronic receiver backends. Next, we calculate the detection sensitivity of an ideal Rydberg sensor operating at the standard quantum limit (acronymized RSQL) at frequencies below 30 MHz. We also derive a prediction for the sensitivity achieved by warm Rydberg vapors and electromagnetically induced transparency (REIT sensor) at the same frequencies. We show that unmatched, active antenna-based circuits outperform REIT sensors, and that both can approach atmospheric noise levels. RSQL sensors offer significant opportunity for improvement beyond state-of-the-art sensitivity, which could enable applications such as precision RF metrology in shielded environments. We present equivalent circuit models that facilitate comparisons between quantum and antenna-based sensors in the electrically small regime, and we conclude by plotting an example comparison for 1 cm-sized sensors in the frequency range of 3×104 to 3×107 Hz. We observe a large performance gap between the sensitivity of current warm-atom-based Rydberg sensors and the fundamental sensitivity predicted by the standard quantum limit, motivating further research in Rydberg sensors.

We begin by calculating the minimum detectable incoming RF field for each sensor type. We consider an incoming plane wave RF field as well as external noise characterized by the amplitude of their respective Poynting vectors S and S̃, as depicted in Fig. 1. We use over symbols to represent noise processes, which are written in spectral density units. For example, S̃ has units of W/(m2 Hz).

FIG. 1.

Radio-frequency (RF) field detector. A plane wave RF field with Poynting vector amplitude S is absorbed by an antenna or atom represented as a light blue dipole antenna. The sensor is also subjected to omnidirectional noise with amplitude S̃. The absorbed field is readout by a back end circuit (green). The minimum detectable RF field is limited by external noise S̃ and equivalent (input-referred) voltage noise inside the sensor Ṽin.

FIG. 1.

Radio-frequency (RF) field detector. A plane wave RF field with Poynting vector amplitude S is absorbed by an antenna or atom represented as a light blue dipole antenna. The sensor is also subjected to omnidirectional noise with amplitude S̃. The absorbed field is readout by a back end circuit (green). The minimum detectable RF field is limited by external noise S̃ and equivalent (input-referred) voltage noise inside the sensor Ṽin.

Close modal
An RF sensor may be limited by either incoming external noise or by internal noise, as shown in Fig. 1. This results in a total signal-to-noise (SNR) density of
(1)
where SNR̃in and SNR̃ex are the internal (in) and external (ex) signal-to-noise ratios, respectively. At the frequencies considered in this paper and in the presence of atmospheric noise, SNR̃ex is often dominant. However, the relative contribution of SNR̃ex can be decreased by, for example, constructing a sensor array. Vin and Ṽex are the Thévenin equivalent voltage amplitudes, and Vin is equivalent to the open circuit voltage for the antenna-based sensors. All signal voltages represent the peak amplitude of oscillating signals at a frequency ω. The minimum detectable Poynting vector amplitude S, with spectral density S̃min, is defined such that SNR̃=1 in a 1 Hz bandwidth.

We treat the scenario depicted in Fig. 1. Because a sensor does not differentiate between incoming noise and signal, the only way to improve SNR̃ex is to increase the antenna (or Rydberg sensor) directivity. Electrically small antennas with high directivity are theoretically possible18 although typically impractical. The antenna gain profile of a Rydberg sensor and a dipole antenna is comparable since we consider atomic transitions where the atom-field interaction is dipolar. Therefore, all sensors considered in this work—including the Rydberg sensor—are assumed to have a directivity equal to that of a dipole, namely, 3/2. Thus, all sensors we consider are equivalent with respect to SNR̃ex.

Given these assumptions, we narrow focus to the internal signal-to-noise ratio, SNR̃in, that quantifies our ability to precisely measure Vin. We calculate the input-referred noise voltage Ṽin. Ṽin is also referred to as noise equivalent voltage (NEV) and is related to the noise equivalent input field (NEF) Ẽmin or B̃min (for a loop) by applying the appropriate field conversion factor.

First, we represent the antenna (either dipole or loop) as a Thévenin equivalent voltage source, a reactance Xa, and a resistance Ra. While the antenna resistance Ra is composed of both the physical loss resistance and the radiation resistance, the radiation resistance is negligible at the frequencies considered in this paper. Figure 2(a) depicts the equivalent circuit for passive backend with load resistance Rl and load reactance Xl. Vout is found by analyzing the RLC circuit with a general result,
(2)
where γ(ω) is the magnitude of voltage gain in the RLC circuit,19 dependent on the carrier frequency ω. We assume that the noise is dominated by Johnson noise from the resistors Ra and Rl, resulting in a total sensor noise of
(3)
where T is the physical temperature of the antenna and kb is Boltzmann's constant. The two terms correspond to Johnson noise emanating from the load resistance Rl and antenna resistance Ra, respectively. λn and γn are the RLC gain experienced by each noise source. Since antenna noise is present at the circuit input, we approximate γnγ and similarly approximate the readout noise gain to one, λn1. For accurate analysis of realistic circuits, γn and λn can be individually calculated or measured. Given these approximations, the resulting NEV from Eq. (3) and these considerations is
(4)
FIG. 2.

Equivalent circuit diagrams for antenna-based and Rydberg RF sensors. (a) Circuit diagram for a passive small antenna (blue box) coupled to an ideal passive receiver backend (green box). (b) Equivalent circuit diagram for an actively readout small antenna. (c) Equivalent circuit for a quantum-limited Rydberg sensor (RSQL sensor).

FIG. 2.

Equivalent circuit diagrams for antenna-based and Rydberg RF sensors. (a) Circuit diagram for a passive small antenna (blue box) coupled to an ideal passive receiver backend (green box). (b) Equivalent circuit diagram for an actively readout small antenna. (c) Equivalent circuit for a quantum-limited Rydberg sensor (RSQL sensor).

Close modal
For an under-damped resonant circuit that is driven near the resonance frequency ω0, γ(ω) is approximately Lorentzian with maximum amplitude given by the quality factor Q. In the limit of small load resistance, this yields a fundamental limit to NEV of
(5)
One significant disadvantage of this resonant and matched regime is the low instantaneous bandwidth of the circuit ωBWω0/Q. The maximum of ωBW for a resonant, passive, and lossless system is given by the Chu-Harrington limit.9,10 Furthermore, matching a small dipole antenna with large capacitive reactance Xa is often impractical (e.g., requires a large inductor).
To treat the unmatched case, one may also perform readout using only a resistor, setting the load reactance Xl to zero. In this case, the circuit forms a voltage divider with complex gain γ(ω)Rl/(Rl+Xa).19 For an electrically small dipole antenna, where Xa is large, the squared NEV is minimized by setting Rl=Xa, resulting in
(6)
This unmatched situation results in a larger NEV than Eq. (5).
Next, we consider the ideal active sensor system of Fig. 2(b), characterized by input voltage noise Ṽamp, amplifier input impedance Ramp, and ideal gain G. The circuit is limited by the voltage divider formed by Xa, Ra, and Ramp. Noise is contributed by Ṽamp and Johnson noise from Ra. The resulting squared NEV is
(7)
If the load impedance Ramp is much greater than the antenna reactance Xa and resistance Ra, and Ṽamp is small, the active dipole-based sensor attains the ideal sensitivity for the small antenna from Eq. (5). However, in realistic systems, Ṽamp often dominates. This scenario also assumes that the active amplifier has enough bandwidth to receive the signal at frequency ω.

Next, we tackle the NEV/NEF of a Rydberg sensor. We first consider the case of an ideal quantum sensor operating at the standard quantum limit (RSQL).6,20 We consider a single Rydberg transition with frequency ω0 and resonant dipole moment d. We take the incoming field with frequency ω to be resonant, ω=ω0. We display the Rydberg sensing circuit model in Fig. 2(c). The results of the circuit model yield the same result, by construction, that would be achieved by considering canonical models for quantum sensors.2,20

The RSQL sensor is modeled as an RLC resonant circuit in the under-damped regime with resonance frequency ω0 and quality factor Q. The resonant circuit is driven with an effective (unitless) voltage Vin, which corresponds with the atom-field interaction. We define this voltage to be
(8)
where d is the dipole moment of the atomic transition. Vin is defined to map, for example, to a small angular evolution on the Bloch sphere.20 The resistor value R, thus the circuit Q, is related to the coherent evolution time τ and decoherence rate Γ of the quantum sensor that integrate the effect of the atom-field interaction Vin, Qω0τeτΓ. The factor of ω0 included in the definitions of Vin and Q makes both quantities unitless. The output of the effective circuit model for the RSQL sensor is Vout=QVin. We note that in reality atomic sensors typically operate in the “rotating wave” regime, which effectively demodulates the incoming signal against a resonant local oscillator. This phenomenon is not treated explicitly in the circuit model of Fig. 2(c), since it is not required to achieve the correct sensitivity analysis.
The RSQL sensor is limited by noise Ṽout arising from random wave-function collapse of N atoms. The amplitude of the input voltage Vin and noise Ṽout is not physical quantities, but is rather defined to be equal to the known result for quantization noise of a quantum sensor operating at the standard quantum limit,6,20
(9)
If the required measurement bandwidth ωBW is less than twice the atom decoherence rate Γ, the optimum evolution time is τ=1/(2Γ).20 Conversely, if ωBW is greater than Γ, we choose τ=1/ωBW. This leads to the following NEV with two different regimes:
(10)
where e is the natural constant. One significant conclusion is that the RSQL sensor is the only sensor considered in this work for which the NEV explicitly depends on sensor bandwidth ωBW. Assuming the required bandwidth is low (ωBWΓ), the NEV may be improved by reducing decoherence Γ.

We take the treatments described in preceding paragraphs and compare the predicted noise equivalent RF fields in Fig. 3. Each of the sensors considered assume a sensing region of approximately 1 cm. Furthermore, to calculate concrete numbers in Fig. 3, several additional assumptions are made including antenna wire dimensions, noise characteristics, and atom number limitations. The supplementary material is included with figure-generating Python source code to allow these choices to be modified for broad exploration.

FIG. 3.

Comparison of minimum detectable Poynting vector S̃min and corresponding minimum detectable E-field Ẽmin for Rydberg and antenna-based RF sensors that are 1 cm in scale. The 10%–90% exceedance band for atmospheric noise referenced to a small dipole antenna is plotted for reference from the ITU Radio Noise recommendations.21 Experimental results from Lei et al.22 and Liu et al.23 are shown as well.

FIG. 3.

Comparison of minimum detectable Poynting vector S̃min and corresponding minimum detectable E-field Ẽmin for Rydberg and antenna-based RF sensors that are 1 cm in scale. The 10%–90% exceedance band for atmospheric noise referenced to a small dipole antenna is plotted for reference from the ITU Radio Noise recommendations.21 Experimental results from Lei et al.22 and Liu et al.23 are shown as well.

Close modal

In order to construct the results for antenna-based sensors, we assume that the antenna resistance arises solely from Ohmic losses. The conductor that makes up the loop and dipole antenna conductor is chosen to be copper with the diameter a=1 mm. The loop is given a diameter d= 1 cm, and the dipole is similarly assigned full length l= 1 cm. The copper conductor resistivity is Rs=1.8×108 Ωm, and the magnetic permeability of the loop core is permeability of free space, μ. For the active circuit, we assume the parameters of a low-noise pre-amp with high input impedance, Ṽamp=1nV/Hz and Ramp=100MΩ. These realistic values are commonly achieved with available amplifiers.

We use Eq. (5) to add the results for matched/passive antennas to Fig. 3 (orange dash, red dot). Because the single-turn loop that we consider only detects the magnetic field derivative, given by Faraday's law, the loop is significantly less sensitive to the incoming Poynting vector at the frequencies considered here. However, loop antennas (often with multiple turns and ferrite cores) offer several practical advantages including easily tunable resonance and relatively easy matching. Conversely, the NEF for the matched dipole starts out frequency independent but rises slightly with frequency due to wire skin depth decreasing with frequency. Although the matched dipole is the most sensitive of the antenna-based sensors, this device suffers significant difficulty in the practicality of lossless matching and the fundamental limitation in bandwidth that results due to the Chu-Harrington limit.9 

Next, we plot the NEFs for unmatched dipoles with passive [blue dash, Eq. (6)] and active (green dot-dash) receiver backends. The unmatched, passive sensor, similar to what was considered in a previous comparison work,2 is the least sensitive of those considered. The active receiver significantly improves performance by reducing the voltage division effect caused by impedance mismatch due to the amplifier's high input impedance. For the values chosen, this active system becomes flat in sensitivity above 100 kHz and is limited solely by the amplifier's input noise. In the near term, this approach is practical and can surpass the sensitivity of current state-of-the-art Rydberg sensors.

To add RSQL sensors to our comparison, we must apply Eqs. (10) and (8), which amounts to choosing an appropriate dipole moment, decoherence rate, and atom number. In choosing these values, we assume tightly packed, cold atoms. The result is plotted as purple dots in Fig. 3. We apply the following process. First, we map out the possible Rydberg transitions in rubidium resonant in the VLF-HF bands, restricting ourselves to quantum numbers l15 and n<100, above which operation is non-optimal. Using the Atomic Rydberg Calculator (ARC),24 we calculate each transition's dipole moment and decoherence rate Γ, including black body induced decay at room temperature. The decoherence rate Γ is of order 2π×1 kHz over the range of the plot, and exact values may be found (and modified) in the supplementary material.

Last, we define the atom number by confining ourselves to a 1 cm3 volume and restricting the density. The density is chosen to be that which limits van der Waals interactions between atoms to less than a 1 MHz frequency shift. This shift is calculated using C6 coefficients from ARC. The atom number is optimized at each frequency, but is of order 108 over the range of the plot. This gives us an idealized view of the capability of Rydberg sensors in this frequency regime, yielding a sensitivity 1011 V/(m Hz) shown as a purple dotted line in Fig. 3. Numerous effects, including resonant dipole–dipole interactions, plasma formation,25 or other collective effects26 may further limit the ideal sensor. Much like the line for an ideal matched dipole, the RSQL sensor is likely to be physically unrealizable but shows a bound of what is possible. Atomic entanglement may lead to additional improvements.20 

Finally, we briefly consider REIT sensors and state-of-the-art experimental demonstrations based on warm vapors. Previous work has calculated the optimal NEF that may be achieved with such sensors,27 and the results are consistent with experimental results,3 resulting in a bounding sensitivity for warm-atom EIT schemes of approximately 106V/(mHz). Recent experiments have further shown that the optimum resonant sensitivity, achieved at microwave frequencies, may be scaled to lower frequencies using high angular momentum states.28–31 

The estimate of optimal NEF for REIT-based sensors is shown as a pink line in Fig. 3. To calculate this line, we linearly scale the optimum REIT sensitivity of approximately 106V/(mHz)3,27 by the dipole transition strengths of available resonant transitions in rubidium 85. The maximum principal quantum number n is capped at 100, and the angular momentum is capped at quantum number l=15. Optimizing within this range results in the jagged nature of the line. Nonetheless, the prediction remains of order 106 V/(m Hz) across the plot range. We consider this prediction to be optimistic and bounding for REIT-based readout, and practical limitations such as cell shielding32 may further limit sensitivity. We also include two data points corresponding to published experimental results within the plotted range.22,23

It is valuable to view Fig. 3 as being made up of two regions. The lower two dotted lines in Fig. 3, corresponding to the ideal matched dipole and the RSQL sensor, are idealizations, and both fall beneath typical atmospheric noise levels. Although these lines will not likely be realized by a physical platform, they, nonetheless, set an important fundamental bound for the technology. In contrast, the lines for the REIT sensor and amplified dipole antenna can likely be achieved in practice and meet the 10% exceedance level for atmospheric noise (blue band) that nominally sets a limit for outdoor communications. Our analysis makes a strong case that unmatched dipole antennas with amplifier readout yield superior performance to what can currently be achieved with REIT sensors. Nonetheless, the large amount of available sensitivity between the two regions of the plot is promising.

While sensors can approach atmospheric noise levels, sufficient for many applications, Rydberg RF sensors may become useful for reasons apart from their sensitivity. Recent demonstrations including simultaneous phase and amplitude detection,33 multi-band reception,34 large dynamic range,35 accurate calibration,36 Tera-Hertz imaging,37 and sub-thermal detection at microwave frequencies38 serve as justification and motivation for further research. New sensing schemes that use a larger effective atom number and reach the standard quantum limit (or beyond, by using entanglement) are an important area for future study. The fact that current Rydberg atom systems are far from the idealized interaction-limited sensitivity is a significant motivation for future research.

See the supplementary material for a zipped folder containing a Jupyter notebook and Python source code to re-create Fig. 3 and modify the parameters to create custom comparisons.

The authors acknowledge useful discussions with Fredrik Fatemi.

Approved for Public Release; Distribution Unlimited. Public Release Case No. 24-1467. The Homeland Security Act of 2002 (Section 305 of PL 107-296, as codified in 6 U.S.C. 185), herein referred to as the “Act,” authorizes the Secretary of the Department of Homeland Security (DHS), acting through the Under Secretary for Science and Technology, to establish one or more federally funded research and development centers (FFRDCs) to provide independent analysis of homeland security issues. MITRE Corp. operates the Homeland Security Systems Engineering and Development Institute (HSSEDI) as an FFRDC for DHS under Contract 70RSAT20D00000001. The HSSEDI FFRDC provides the government with the necessary systems engineering and development expertise to conduct complex acquisition planning and development; concept exploration, experimentation, and evaluation; information technology, communications and cyber security processes, standards, methodologies, and protocols; systems architecture and integration; quality and performance review, best practices, and performance measures and metrics; and independent test and evaluation activities. The HSSEDI FFRDC also works with and supports other federal, state, local, tribal, public, and private sector organizations that make up the homeland security enterprise. The HSSEDI FFRDC's research is undertaken by mutual consent with DHS and is organized as a set of discrete tasks. This report presents the results of research and analysis conducted under: 70RSAT22FR0000021, “DHS Science and Technology Directorate TCD Quantum Information Science Capabilities.” The results presented in this report do not necessarily reflect official DHS opinion or policy.

The views, opinions, and/or findings expressed are those of the authors and should not be interpreted as representing the official views or policies of the Department of Defense or the U.S. Government.

The authors from The MITRE Corporation also acknowledge support from the MITRE Independent Research and Development Program.

The authors have no conflicts to disclose.

K. M. Backes: Conceptualization (lead); Data curation (lead); Formal analysis (lead); Investigation (lead); Methodology (lead); Writing – original draft (lead); Writing – review & editing (lead). P. K. Elgee: Conceptualization (supporting); Formal analysis (equal); Writing – original draft (supporting); Writing – review & editing (supporting). K.-J. LeBlanc: Conceptualization (supporting); Formal analysis (supporting). C. T. Fancher: Conceptualization (supporting); Supervision (supporting); Writing – review & editing (supporting). D. H. Meyer: Conceptualization (equal); Supervision (supporting); Writing – review & editing (supporting). P. D. Kunz: Conceptualization (supporting); Project administration (supporting); Supervision (supporting); Writing – original draft (supporting); Writing – review & editing (supporting). N. Malvania: Conceptualization (supporting); Investigation (supporting). K. L. Nicolich: Conceptualization (supporting); Writing – review & editing (supporting). J. C. Hill: Conceptualization (supporting); Writing – original draft (supporting); Writing – review & editing (supporting). B. L. Schmittberger Marlow: Conceptualization (supporting); Supervision (supporting); Writing – original draft (supporting); Writing – review & editing (supporting). K. C. Cox: Conceptualization (lead); Formal analysis (lead); Investigation (lead); Methodology (lead); Project administration (lead); Supervision (lead); Writing – original draft (lead); Writing – review & editing (lead).

The data that support the findings of this study are available within the supplementary material.

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