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  • Article
  • Open Access

7 March 2026

36 Pages

Operational Threat Modeling of Adversarial Disturbances in Continuous-Variable Quantum Communication

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1
Department of Mechanical and Mechatronics Engineering, University of Waterloo, Waterloo, ON N2L 3G1, Canada
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LAKES Environmental Research Inc., Waterloo, ON N2L 3L3, Canada
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Applied Quantum Technologies (AQT) Initiative, Columbia, MD 21046, USA
4
EigenQ, Inc., Austin, TX 78701, USA

Abstract

Continuous-variable quantum communication (CVQC) relies on finite-window estimation of phase space moments, making receiver decisions sensitive to finite measurement resolution, calibration uncertainty, and confidence-calibrated tolerances. This paper develops a receiver-centric threat modeling framework for structured (including adversarial) physical-layer disturbances under finite-sample inference. We introduce an operational taxonomy, reconnaissance, exploratory, and denial-of-service, defined by statistical visibility relative to acceptance regions rather than by assumed physical mechanisms. Using an effective estimator space Gaussian model r ^ ′ = G r ^ + ξ with additive covariance N, we show how distinct mechanisms can be observationally equivalent within finite tolerances and we propose a protocol-agnostic scalar severity coordinate Δ E based on the covariance trace. We derive χ 2 -based missed-detection expressions and a soft detectability boundary scaling as 1 / n , and we corroborate the predicted P miss ( ν ) behavior via Monte Carlo simulations across representative block sizes. The resulting framework clarifies the delimitation from conventional CV-QKD excess noise parameterization and provides a structured basis for monitoring-layer design and comparative threat-taxonomy mapping.

1. Introduction

Recent advances in quantum communication have made it increasingly clear that security and integrity are shaped not only by idealized theoretical guarantees, but also by operational constraints such as finite measurement resolution, estimator tolerances, and hardware-imposed control limits. In particular, our prior work demonstrated that finite-resolution measurements can induce regions of operational indistinguishability, termed convergence vicinities, in which distinct physical models become experimentally indistinguishable without violating Bell’s theorem itself [1]. That analysis exposed a class of implementation-level vulnerabilities in integrity verification frameworks that rely on static thresholds or idealized measurement assumptions. We emphasize that [1] treats discrete-variable integrity verification under finite-resolution indistinguishability, whereas the present manuscript develops a continuous-variable, receiver-observable threat modeling framework for CVQC based on covariance-level monitoring, regime taxonomy, and finite-sample visibility. The shared element is the receiver-centric tolerance/indistinguishability viewpoint, while the technical setting and observables differ (discrete outcomes vs. covariance-level monitoring).
The present work extends this operational perspective to continuous-variable quantum communication (CVQC), where receiver decisions are driven directly by finite-resolution estimates of phase space statistics. Unlike discrete-variable integrity checks, CVQC systems infer performance- and (when applicable) security-relevant parameters from continuous-valued estimators, quadrature variances, covariances, and covariance matrices, that are intrinsically subject to finite-sample uncertainty and confidence-region design.
In CVQC, quantum information is encoded in the canonical quadratures of optical modes and accessed experimentally via homodyne or heterodyne detection. Rather than treating noise exclusively as an uncontrolled environmental process, we consider adversarial disturbances: intentional, structured perturbations designed to exploit estimator tolerances, probe stability margins, or disrupt communication. For clarity and to reduce repetition, terminology is consolidated in Table 1. Such interference need not appear as anomalously large fluctuations; it can be engineered to remain within nominal operating margins over typical monitoring windows while gradually biasing parameter estimation, degrading coherence, or undermining operational assumptions.
Table 1. Terminology used in this manuscript.
CVQC plays a central role in quantum communication and networking due to its compatibility with existing optical infrastructure and its scalability [2,3,4]. At the same time, practical CVQC implementations are sensitive to excess noise, phase instability, and detector limitations, which can compromise inferred channel parameters and communication reliability, especially under finite-size parameter estimation constraints [5,6,7,8,9,10,11,12]. These sensitivities define a physical-layer threat surface in which disturbances can be shaped to interact with acceptance criteria and estimator uncertainty [13,14,15,16].
In this work, we classify adversarial interference in CVQC into three operational regimes. Reconnaissance disturbances are low-amplitude perturbations engineered to remain within estimator tolerances while extracting information about system parameters. Exploratory disturbances introduce moderate, structured perturbations intended to probe stability margins and reveal directional sensitivities in phase space. Finally, denial-of-service (DoS) disturbances correspond to high-intensity interference that overwhelms estimation and control capabilities, forcing operational failure. Throughout this work, covariance matrices are expressed in shot-noise units (vacuum variance normalized to unity), and proportionality constants relating energy and covariance trace are omitted for clarity.
To analyze these regimes in an implementation-relevant manner, we adopt a receiver-centric modeling perspective based on an effective Gaussian channel description acting on phase space quadratures. Within this framework, we characterize how disturbances perturb second-order moments accessible to the receiver and how such perturbations translate into estimator degradation and operational failure risk under finite-sample constraints. We introduce an energy deviation metric derived from the covariance trace, providing a compact scalar observable that links disturbance-driven covariance inflation to tolerance design and failure thresholds. Figure 1 provides a receiver-centric schematic of the operational threat surface and the effective estimator-space interpretation of ( G , N ) used throughout this work.
Figure 1. Receiver-centric operational threat surface for continuous-variable quantum communication. Schematic diagram (not to scale): Arrows indicate conceptual points of adversarial influence (e.g., phase reference manipulation, injected disturbances/jamming, detector/ADC saturation), while receiver decision logic is based on finite-resolution estimators of first- and second-order quadrature moments (mean/covariance). The pair ( G , N ) denotes the total observable effect inferred at the receiver and need not coincide with the adversary’s physical mechanism or implementation. The diagram provides an operational interpretation of the effective Gaussian channel model in Equation (1), not a specific hardware layout. Simulation-based missed-detection curves are provided later (Section 3.8) to complement the schematic regime illustrations.
This manuscript focuses on receiver-observable operational threat modeling. It provides a regime taxonomy and observable-level characterization of adversarial interference, but it does not constitute a protocol security proof, a mitigation design, or a prescriptive detection mechanism. In particular, the mapping from a physical disturbance to inferred effective parameters ( G , N ) in Equation (1) (Section 3) is generally non-identifiable without additional instrumentation or assumptions because distinct mechanisms can induce statistically indistinguishable changes in finite-sample covariance estimates. The regimes defined here should therefore be interpreted as operational equivalence classes in estimator space. We also discuss the consequences of allowing estimator space G that is not constrained to be physically realizable and how physical plausibility constraints can be imposed when desired (Section 3).
Specifically, this work makes three contributions: (i) it formalizes a taxonomy of adversarial disturbance regimes in CVQC grounded in operational intent and estimator visibility; (ii) it develops a Gaussian channel modeling framework that captures adversarial interference at the level of receiver-accessible covariance statistics without assumptions about adversary capabilities; and (iii) it introduces an energy deviation metric and finite-sample detectability analysis that connect disturbance-driven covariance inflation to estimator tolerances and operational failure boundaries. To complement the analytic visibility bounds, we include Monte Carlo simulation plots that corroborate the predicted missed-detection behavior and its scaling under the stated i.i.d. baseline assumptions (Section 3.8). Together, these results establish a structured, receiver-centric foundation for analyzing physical-layer adversarial behavior in continuous-variable quantum communication.
Remark 1 
(Normalization convention used throughout). Unless stated otherwise, we use shot-noise unit (SNU) normalization in which the vacuum variance is unity, i.e., for a single mode V vac = I 2 (and for m modes V vac = I 2 m ). All covariance matrices, tolerances, and energy deviation quantities in this paper are expressed relative to this convention.

3. Receiver-Observable Modeling of Adversarial Disturbances

From a cybersecurity perspective, adversarial disturbances in CVQC constitute a physical-layer attack surface: structured perturbations can exploit estimator tolerances, control assumptions, and finite-resolution effects by acting on the receiver’s inference layer and decision margins.
In continuous-variable (CV) quantum systems, quantum information is encoded in the canonical quadratures x ^ and p ^ of optical modes. These quadratures fully characterize Gaussian quantum states and form the operational foundation of CVQC systems and devices [4]. As a result, performance- and integrity-relevant information in CVQC is inferred from finite-resolution measurements of phase space observables and from finite-sample estimators built from those measurements.
At an operational level, adversarial disturbances are modeled as an effective Gaussian channel acting on the phase space vector r ^ = ( x ^ , p ^ ) T :
r ^ ′ = G r ^ + ξ ,
where r ^ and r ^ ′ denote the input and receiver-observed output phase-space vectors, respectively; G is a real linear transformation on phase space representing deterministic effects such as attenuation, amplification, rotation, or effective squeezing, as inferred from receiver-accessible observables; and ξ is a classical random vector drawn from a zero-mean Gaussian distribution with covariance matrix N. This representation is used as a phenomenological description of receiver-observable impact, not as a claim about the adversary’s physical implementation or resources. In particular, G is not assumed to correspond to a physically realized or symplectic operation, and the model does not assume coherent quantum control by the adversary. Equation (1) is applied at the level of per-window receiver statistics and can be instantiated with time-varying ( G ( t ) , N ( t ) ) for non-stationary disturbances. The finite-n detectability formulas later in the paper use an i.i.d. baseline within a window and are accompanied by a correlation/ n eff sensitivity discussion (Section 3.8 and Section 4).
  • Physical plausibility versus estimator space effectiveness
  • Because G is not constrained here, the pair ( G , N ) can represent estimator space effective behavior that would not correspond to a physically realizable Gaussian quantum channel. If one wishes to restrict to physically realizable single-mode Gaussian channels, ( G , N ) can be constrained by the standard complete-positivity condition N + i ( Ω − G Ω G T ) ⪰ 0 , with Ω = 0 1 − 1 0 (see standard Gaussian channel references, e.g., [4]). Operationally, one may (i) enforce this constraint during fitting of ( G ^ , N ^ ) , or (ii) project an unconstrained estimate onto the nearest feasible physical set, if physical attribution is required. The present manuscript does not enforce such constraints because its goal is to characterize receiver-visible regime behavior and tolerance-induced indistinguishability, not to uniquely identify an underlying mechanism.
  • Scope of the Gaussian channel model
  • Equation (1) summarizes the net impact of disturbances as inferred from finite-resolution estimates of first- and second-order quadrature moments. It does not assert that an adversary implements a Gaussian or symplectic physical process, and it may not capture attack signatures that manifest primarily in higher-order moments, non-Gaussian tails, or strongly nonlinear detector effects. Limitations of this covariance-level view are summarized in Section 4.
In this receiver-centric view, the parameters ( G , N ) summarize the net observable impact of upstream disturbances on the statistics used by the receiver’s estimator and acceptance tests, and therefore on tolerance-induced decision boundaries.
Distinct adversarial strategies correspond to different effective choices of G and N, reflecting both the intensity and operational intent of the interference. Throughout this work, adversarial disturbances are treated as an operational class characterized by receiver-side statistical signatures, independent of assumptions about adversary hardware or attack mechanism.
Remark 2 
(Receiver-observable modeling and non-identifiability). The pair ( G , N ) in Equation (1) is an effective description of disturbance impact as seen through receiver estimators. In general, different physical-layer mechanisms can yield statistically indistinguishable ( G ^ , N ^ ) within finite confidence regions, so this framework does not claim mechanism identification. To reduce repetition, we treat this as a standing interpretive caveat established in Section 1 and do not restate it elsewhere unless needed for a specific derivation.

3.1. Receiver Observables and Estimator Tolerances

The operational impact of adversarial disturbances in continuous-variable quantum communication is determined not only by the physical disturbance applied to the channel, but by how that disturbance manifests in receiver-accessible observables under the receiver’s finite-resolution, finite-sample inference pipeline. In practice, integrity assessment, calibration, and performance verification in CVQC rely on windowed, finite-sample estimates of quadrature moments derived from homodyne or heterodyne measurements with limited resolution and detector noise.
At the receiver, experimentally accessible information is typically restricted to first- and second-order moments of the quadratures, summarized by an estimated mean vector and covariance matrix. These estimates are subject to statistical uncertainty arising from finite-data acquisition, detector inefficiencies, and coarse-graining effects. As a result, any verification or monitoring procedure implicitly defines estimator tolerances: bounded regions in parameter space within which observed statistics are deemed consistent with nominal operation at a chosen false-alarm level.
Adversarial disturbances can exploit these tolerances by shaping perturbations so that their induced changes in observable statistics remain within accepted confidence regions over typical monitoring windows. In this sense, the adversary interacts with the receiver’s inference layer and its tolerance-calibrated decision logic, rather than with an idealized, infinitely resolved state description.
Formally, let V ^ denote the estimated covariance matrix obtained from a finite ensemble of measurements. Acceptance regions for nominal operation can be represented as
∥ V ^ − V ref ∥ ≤ δ V ,
where V ref is a reference covariance matrix and the norm may be interpreted operationally as a chosen matrix norm (e.g., the Frobenius norm) or, equivalently, as a set of elementwise confidence bounds on estimated covariance entries. The tolerance δ V is determined by finite-sample size, measurement resolution, and the receiver’s confidence-level design. Perturbations that induce changes smaller than δ V are operationally invisible over that window, even if they introduce systematic bias or accumulate deleterious effects over time (cf. long-horizon drift discussion in Section 3.8).

3.1.1. Tolerance, Threshold, and Acceptance Region

Definition 1 
(Tolerance, threshold, acceptance region). Let θ ^ be a receiver estimator (e.g., a variance, a covariance entry, Tr ( V ^ ) ) with nominal reference value θ ref . A tolerance δ θ ( α ) is a confidence-calibrated margin such that Pr ( | θ ^ − θ ref | ≤ δ θ ( α ) ∣ θ = θ ref ) ≥ 1 − α . The associated acceptance region is
A θ ( α ) : = { θ ^ :   | θ ^ − θ ref | ≤ δ θ ( α ) } .
A threshold is a decision cut-off used to declare failure/abort (e.g., an operational limit Δ E th ) and is conceptually distinct from estimator tolerances, though in practice, thresholds are often chosen relative to tolerance-calibrated acceptance regions. Here, Tr ( · ) denotes the matrix trace and A θ ( α ) denotes the acceptance region for θ ^ at significance level α.

3.1.2. Setting δ est , δ V , and δ e from Confidence Levels

Unless stated otherwise, we parameterize tolerances by a one-sided significance level α (false-alarm target) and the window sample size n, i.e., δ est = δ est ( α , n ) , δ V = δ V ( α , n ) , and δ e = δ e ( α , n ) , with α selected by receiver design and n determined by the monitoring window/block size.
The χ 2 /Wishart finite-sample laws used below are classical results; the contribution here is their operational use to define tolerance-induced stealth bands and regime boundaries for receiver-side CVQC monitoring under structured disturbances.
  • Variance tolerance δ est (one-sided)
  • For p i ∼ N ( 0 , σ 0 2 ) , the known-mean estimator σ ^ 2 = 1 n ∑ i = 1 n p i 2 obeys the finite-sample law Equation (29) (Section 3.8.1). A one-sided ( 1 − α ) acceptance test can be written as
    σ ^ 2 ≤ σ 0 2 + τ α ,   τ α : = σ 0 2 χ n , 1 − α 2 n − 1 ,
    so that δ est may be taken as τ α plus any additional resolution/calibration margin and any guard band used by the receiver.
  • Covariance matrix tolerance δ V
  • For 2 m -dimensional Gaussian samples with true covariance V, the sample covariance (mean-corrected) V ^ satisfies ( n − 1 ) V ^ ∼ W 2 m ( V , n − 1 ) (Wishart distribution). Operationally, one can construct an acceptance region either (i) entrywise via simultaneous confidence bounds, or (ii) as a matrix norm ball ∥ V ^ − V ref ∥ F ≤ δ V ( α ) . In practice, δ V ( α ) is set from calibration data (nominal operation) by choosing the smallest radius that achieves a target false-alarm probability α under the receiver’s sampling and digitization pipeline, thereby incorporating non-idealities such as digitizer quantization and detector noise.
  • Energy deviation tolerance δ e
  • Because the energy deviation induced by disturbances is Δ E = Tr ( V ′ ) − Tr ( V 0 ) / 4 , as defined in Equation (18) (Section 3.7.1), a trace-based acceptance test
    Tr ( V ^ ) ≤ Tr ( V ref ) + τ E
    induces the scalar tolerance
    δ e : = τ E 4 .
For near-vacuum-normalized operation (diagonal-dominant V) and large n, conservative scaling is Std ( Tr ( V ^ ) ) = O ( ∥ V ∥ F / n ) , so τ E (and therefore δ e ) inherits the same 1 / n finite-sample behavior as Equation (31) (Section 3.8.1), up to constants determined by calibration and windowing choices.

3.1.3. Correlation-Aware Interpretation via an Effective Sample Size n eff

The tolerance expressions above are stated for an i.i.d. baseline within a monitoring window. In deployed links, temporal correlations (e.g., due to phase reference dynamics, drift, or control loops) reduce statistical resolution relative to the nominal window length n. A standard proxy is an effective sample size n eff ≤ n , which yields the leading-order substitution n ↦ n eff in 1 / n scaling laws (and therefore widens tolerance-induced stealth bands). We quantify this sensitivity and provide a simple illustrative mapping (including an AR(1) example) in Section 3.8.5.
This receiver-centric viewpoint motivates the modeling choices adopted throughout this work. Rather than characterizing adversarial disturbances by physical origin, we classify them by observable impact relative to estimator tolerances. Reconnaissance, exploratory, and denial-of-service regimes are then distinguished by how their induced covariance distortions relate to acceptance regions and failure thresholds.
In later sections, we use τ as a scalar analogue of δ V for variance-based monitoring, and δ est as a generic tolerance scale when the specific estimator is not explicitly specified, with the understanding that τ ≡ τ α when set by a target false-alarm level.

3.2. Summary of Adversarial Regimes

For clarity and implementation relevance, Table 5 summarizes the three adversarial disturbance regimes considered in this work in terms of (i) operational intent, (ii) characteristic intensity relative to estimator tolerances, (iii) dominant observable signatures in receiver-side quadrature statistics, and (iv) expected operational consequence for continuous-variable quantum communication (CVQC). This summary emphasizes that regimes are defined operationally by how disturbances manifest in experimentally accessible observables under finite-window estimation, rather than by assumptions about an adversary’s physical resources or internal attack mechanism.
Table 5. Operational summary of adversarial disturbance regimes in CVQC. Regimes are distinguished by adversarial intent and by their characteristic impact on receiver-side quadrature statistics and estimator reliability.
These regime boundaries should be interpreted as receiver-defined surfaces in estimator space, determined by measurement resolution, sample size, estimator design, and acceptance criteria, rather than as intrinsic thresholds of the underlying physical disturbance. Therefore, the regime boundaries in Table 5 are operational rather than absolute: the same physical perturbation may transition between regimes depending on device characteristics, finite-sample uncertainty, and application-specific failure thresholds. This perspective motivates the use of receiver-side covariance statistics, and in particular, the energy deviation metric introduced in Section 3.7.1, as a protocol-agnostic means of quantifying proximity to tolerance and failure boundaries.

Relation to CV-QKD Excess Noise Parameterization and Abort Logic

In CV-QKD, parameter estimation typically produces confidence bounds on channel transmittance and excess noise (often denoted ξ in shot-noise units), which are then used to compute a finite-size (and, in composable treatments, explicitly bounded) security margin and to decide accept/abort [6]. A common operational rule is to abort key generation when a worst-case (upper) estimator ξ U exceeds a protocol-dependent maximum tolerable value ξ max (equivalently, when the inferred finite-size key rate becomes non-positive).
  • Formal delimitation
  • The present work does not reintroduce excess noise estimation under new terminology. Instead, it generalizes the monitoring-layer viewpoint: acceptance regions are treated as explicit receiver decision surfaces that induce tolerance-defined indistinguishability bands, and adversarial regimes are defined by estimator visibility relative to those surfaces. Conventional CV-QKD parameter estimation is recovered as a special case when one restricts the effective estimator space model (Equation (1)) to physically motivated channel parameterizations and interprets acceptance/abort purely through ( T , ξ ) confidence bounds.
  • Operational mapping of regimes
  • Under this interpretation, (i) reconnaissance corresponds to disturbances that keep ξ U (or Tr ( V ^ ) ) within the acceptance region A ( α ) over typical monitoring windows; (ii) exploratory corresponds to disturbances that push estimates toward the acceptance boundary (intermittent detectability and stress without immediate abort); and (iii) DoS corresponds to disturbances that rapidly drive ξ U ≫ ξ max or induce estimator/hardware breakdown, forcing abort/failure. Therefore, this paper extends the accept/abort logic beyond QKD to CVQC broadly by focusing on receiver-accessible covariance statistics and finite-window visibility, rather than on protocol-specific secret-key-rate expressions.

3.3. Illustrative Example: Quadrature-Biased Disturbance

To illustrate how the operational regimes defined above map onto receiver-accessible statistics, we consider a simple example of quadrature-biased excess noise. The purpose is not to model a specific attack implementation, but to show how structured disturbances project onto phase space second moments and how the resulting regime classification depends on disturbance magnitude relative to estimator tolerances.
Figure 3 visualizes the regime taxonomy using covariance ellipses (equivalently, Wigner function contours) together with the associated energy deviation scale Δ E ∝ Tr ( V ′ ) − Tr ( V 0 ) . The tolerance level δ e denotes a receiver-defined energy deviation margin (a scalar analogue of the covariance tolerance δ V ), derived from the receiver’s finite-sample acceptance rule (e.g., Equation (32) and the associated confidence level) and any additional resolution/calibration uncertainty. Under this interpretation, regime transitions correspond to changes in the statistical visibility of covariance distortions relative to δ e , rather than changes in physical mechanism.
We consider a single-mode Gaussian state with covariance matrix
V 0 = σ x 2 0 0 σ p 2 ,
where σ x 2 = σ p 2 = 1 for the vacuum reference state. Adversarial interference is modeled as additive excess noise injected preferentially along the momentum-like quadrature
V ′ = σ x 2 0 0 σ p 2 + ν ,
with ν ≥ 0 denoting the magnitude of the quadrature-biased disturbance.
  • Reconnaissance regime
  • When ν is chosen such that ν ≪ δ est , where δ est denotes the effective estimator tolerance imposed by finite-sample size and detector resolution, the induced change in covariance remains within accepted confidence intervals for a typical monitoring window. At this level, the energy deviation
    Δ E ∝ Tr ( V ′ ) − Tr ( V 0 ) ,   Tr ( V ′ ) − Tr ( V 0 ) = ν
    is not statistically resolvable on short timescales. Nevertheless, repeated application of sub-threshold perturbations can bias inferred channel parameters and probe sensitivities without triggering a per-window acceptance test.
  • Exploratory regime
  • For intermediate values of ν , comparable to (or modestly exceeding) estimator tolerances, the covariance matrix becomes measurably anisotropic. Observable consequences include elongation along the p-quadrature and increased sensitivity to phase space orientation. In this regime, rotations primarily redistribute anisotropy across quadrature-resolved observables (e.g., σ ^ x 2 , σ ^ p 2 , V ^ x p ), producing phase-dependent changes in which statistics exceed their tolerances; by contrast, the trace-based energy deviation Δ E remains invariant under ideal rotations. Such behavior reveals directional sensitivities and proximity to stability boundaries while preserving operability (i.e., before abort/failure thresholds are crossed).
  • Denial-of-service regime
  • When ν is increased such that ν ≫ δ est and exceeds device- or protocol-level operating limits, the excess variance dominates the covariance structure. The resulting energy deviation grows rapidly, state purity collapses, and quadrature statistics become incompatible with reliable parameter estimation or communication. In practice, this regime may also coincide with nonlinear receiver effects such as saturation or clipping.
This simplified example highlights three points. First, a single disturbance family can realize different regimes depending on magnitude relative to estimator tolerances and operational thresholds. Second, quadrature bias naturally induces anisotropy, making degradation orientation dependent in the exploratory regime. Third, receiver-side covariance statistics, and the energy deviation metric in particular, provide a compact operational lens for organizing disturbance impact without requiring mechanism identification.

3.4. Reconnaissance Disturbances

Reconnaissance disturbances consist of low-amplitude perturbations deliberately engineered to remain within estimator tolerances while extracting information about system parameters over time. This regime is characterized by stealth: the adversary seeks to avoid triggering integrity checks or anomaly detection mechanisms while accumulating statistically meaningful information across repeated observations.
In continuous-variable systems, reconnaissance disturbances can be represented (at the level of receiver-observable first and second moments) as an effective additive Gaussian perturbation with small variance:
x ^ ′ = x ^ + ϵ x ,   p ^ ′ = p ^ + ϵ p ,
where ϵ x , ϵ p ∼ N ( 0 , σ recon 2 ) and σ recon 2 is chosen to lie below tolerance margins imposed by finite measurement resolution and parameter estimation uncertainty. This is an estimator space representation: it summarizes the net perturbation seen in estimated moments and does not identify a unique physical mechanism. At the level of individual monitoring windows, such perturbations can be experimentally indistinguishable from benign fluctuations. However, when applied persistently, they can introduce systematic bias into inferred system parameters and can produce long-horizon drift in summary observables such as Tr ( V ^ ) or Δ E ( t ) even when per-window tests accept nominality.

Implications for Quantum Communication Protocols and Devices

In practical CVQC protocols and devices, integrity and performance verification rely on parameter estimation performed with finite-sample sizes, finite detector resolution, and predefined acceptance margins for calibration error, loss, and excess variance. Reconnaissance disturbances leverage these operational constraints by introducing small, structured perturbations that do not violate acceptance criteria on a per-window basis, yet gradually bias inferred parameters and operating points.
These effects arise at the implementation level and do not contradict protocol guarantees; rather, they undermine the conditions under which parameter estimation faithfully reflects channel/device behavior. Small excess variance contributions that remain within confidence-calibrated acceptance regions may accumulate over time, shifting estimated operating points without triggering alarms. Operationally, this is the distinction between (i) instantaneous acceptability under a per-window tolerance test and (ii) cumulative bias that becomes visible only through longer-horizon aggregation, drift monitoring, or tighter finite-size confidence accounting.
As demonstrated in the discrete-variable context in [1], verification frameworks based on static thresholds can fail to detect adversarial behavior engineered to remain within acceptance margins. In continuous-variable systems, reconnaissance disturbances can similarly bias calibration, stability assessment, or performance metrics while remaining operationally inconspicuous over typical windows.
Figure 4 emphasizes that reconnaissance disturbances can be operationally stealthy even when each injected perturbation remains below the instantaneous tolerance δ e over short monitoring windows. In this regime, Δ E ( t ) may exhibit gradual upward drift due to repeated sub-threshold injections, causing delayed detection only when a cumulative threshold (or long-horizon alarm criterion) is exceeded.
From an operational monitoring perspective, this distinction naturally connects to sequential change detection and drift monitoring ideas: per-window acceptance tests control false alarms at level α , while long-horizon criteria (e.g., CUSUM-style statistics) can detect persistent small shifts that are individually sub-threshold [22,23].
Finally, because finite-window inference can be correlation-limited, reconnaissance-scale visibility should be interpreted in terms of an effective sample size n eff when temporal correlations are present; this widens tolerance-induced stealth bands relative to the i.i.d. baseline (Section 3.8.5).

3.5. Exploratory Disturbances

Exploratory disturbances correspond to moderate, structured perturbations intended to probe the stability limits of a quantum communication system. Unlike reconnaissance disturbances, which are engineered to remain strictly below tolerance-induced acceptance boundaries, exploratory disturbances are designed to induce measurable, yet non-catastrophic, deviations in receiver-observable behavior. The objective at this stage is not immediate disruption, but to observe how the system responds to controlled stress, thereby identifying sensitivities, nonlinearities, and potential failure modes. Operationally, exploratory disturbances form part of an attacker learning loop, in which injected perturbations are correlated with observable system responses to infer stability margins and response characteristics within the receiver’s estimator space and finite-window acceptance regions.
In continuous-variable systems, exploratory disturbances can be modeled operationally as a Gaussian channel combining moderate additive excess variance with phase space distortion:
r ^ ′ = R ( ϕ ) r ^ + ξ exp ,
where R ( ϕ ) denotes a phase space rotation by angle ϕ , and ξ exp ∼ N ( 0 , N exp ) represents an additive Gaussian term with covariance matrix N exp . The covariance N exp exceeds typical environmental levels but remains below denial-of-service intensity. This phenomenological model captures exploratory interference, including phase reference perturbation and structured excess variance injection, without assuming a specific adversarial implementation. Equivalently, in the receiver-observable ( G , N ) model of Equation (1), exploratory behavior corresponds to effective transformations with a nontrivial G (e.g., rotation/mixing) and/or a moderate additive term N that pushes receiver estimators toward (but not catastrophically beyond) tolerance-induced boundaries.
In contrast to reconnaissance disturbances, exploratory perturbations produce observable distortions in quadrature statistics and state covariance while typically remaining compatible with continued operation, enabling repeated observation of system behavior under stress. From an adversarial perspective, this regime supports systematic probing of how receiver-observable quantities respond to controlled perturbations across operating conditions. Exploratory behavior is naturally characterized by a soft detectability boundary: it corresponds to disturbance levels for which the per-window missed-detection probability P miss ( ν ) is no longer close to unity, yet operational thresholds are not exceeded. We provide simulation-based P miss ( ν ) curves for multiple n in Section 3.8 to illustrate this transition quantitatively.

3.5.1. Impact on System Stability

Exploratory disturbances impact system stability in several operationally significant ways:
  • Phase space asymmetry and mixing. Moderate phase rotations and excess variance introduce asymmetric distortions in the estimated covariance, revealing directional sensitivities in phase space and dependence on operating points (e.g., growth of off-diagonal terms V ^ x p under imperfect phase tracking, or anisotropic eigenvalue inflation before large trace growth).
  • Dynamic response characteristics. Window-to-window changes in estimated quadrature statistics under exploratory perturbations expose characteristic response times, relaxation behavior, and transient dynamics (including variability exploitable to infer effective control loop bandwidth, estimator robustness, and stability margins).
  • Stability margin identification. By varying the magnitude and structure of injected perturbations, exploratory disturbances can reveal regions in parameter space where degradation accelerates, signaling proximity to instability or failure (e.g., onset of estimator instability, increased variability of V ^ across windows, or sensitivity of Δ E to modest increases in N exp ).
These effects allow an adversary to construct an empirical map of system robustness, analogous to stress-testing and vulnerability discovery in classical engineered systems, translated here into phase space dynamics and receiver-side estimators for continuous-variable quantum devices.

3.5.2. Exploratory Disturbances as a Precursor to Escalation

Exploratory disturbances serve as an intermediate stage between stealthy reconnaissance and overt denial-of-service interference. Information extracted during this phase, including sensitivity to phase distortions, tolerance to excess variance, and the onset of nonlinear or unstable behavior, can inform the design of subsequent, higher-intensity perturbations.
As such, exploratory disturbances play a critical role in adversarial escalation strategies. They bridge low-amplitude covert probing and overt disruption by enabling targeted refinement of perturbation parameters based on observed system behavior. In continuous-variable quantum communication systems, this progression highlights the importance of understanding not only failure modes, but also structured pathways through which adversarial interference can evolve from benign-appearing perturbations into destabilizing attacks. Operationally, escalation corresponds to pushing receiver estimates from near-boundary stress (exploration) to threshold exceedance (DoS), as quantified by tolerance-scaled metrics such as ν / δ est and by trace-based deviation Δ E relative to receiver-defined failure limits, with correlation-limited settings interpreted via n eff rather than the nominal n (Section 3.8.5).

3.6. Denial-of-Service (DoS) Disturbances

Denial-of-service (DoS) disturbances represent the most severe class of adversarial interference considered in this work. They are characterized by high-intensity perturbations that overwhelm the CVQC link and render reliable transmission or verification impossible. Unlike reconnaissance or exploratory disturbances, which aim to extract information or probe system stability while preserving operability, DoS disturbances are explicitly disruptive and seek to force operational failure. In this regime, the primary effect of interest is not gradual performance degradation, but rapid breakdown of state integrity and communication viability as reflected in receiver-accessible estimators leaving tolerance-induced acceptance regions and crossing operational abort/failure thresholds.
In continuous-variable quantum communication systems, DoS interference can be modeled operationally as an effective Gaussian channel with large excess variance and/or strong phase diffusion:
r ^ ′ = R ( ϕ ) r ^ + ξ DoS ,
where the phase parameter ϕ may fluctuate rapidly over a wide range, and ξ DoS ∼ N ( 0 , N DoS ) is a Gaussian term with covariance matrix N DoS far exceeding nominal operating limits. This phenomenological model captures intense optical jamming, severe phase reference destabilization, or broadband disturbance injection without assuming a specific adversarial mechanism or implementation. In the receiver-centric ( G , N ) description of Equation (1), DoS corresponds to effective parameters for which either (i) the additive term N dominates second moments (large Tr ( N ) and rapidly growing Tr ( V ^ ) ), and/or (ii) the inferred linear action G induces strong mixing/distortion that renders covariance estimation unreliable within the receiver’s finite-resolution pipeline. Because ( G , N ) is used here in an estimator space sense, extremely large fitted values can in principle correspond to non-physical parameterizations; in DoS settings, this is often operationally immaterial (the receiver fails regardless), but physically plausible modeling can be enforced by constraining ( G , N ) to the Gaussian channel feasibility set if physical attribution is required (Section 3).

3.6.1. Impact on Quantum State Coherence

DoS disturbances rapidly degrade quantum state coherence by dramatically inflating quadrature variances and distorting the phase space distribution. Under the Gaussian receiver model, the covariance matrix V transforms as
V ′ = R ( ϕ ) V R T ( ϕ ) + N DoS ,
leading to a substantial increase in Tr ( V ) . Because the trace of the covariance matrix is proportional to mean energy/variance content under the SNU normalization used throughout (Section 3.7.1), this corresponds to rapid growth in state energy and, operationally, to rapid inflation of receiver-side variance and covariance estimators.
In phase space, this manifests as extensive spreading of the Wigner function and severe reduction in state purity. The nonclassical correlations and phase-sensitive structure required for quantum communication and information-processing tasks are rapidly destroyed, rendering the state unsuitable for reliable transmission, verification, or further processing. At the receiver interface, DoS conditions may also induce non-Gaussian/nonlinear measurement artifacts (e.g., clipping or saturation), in which case, covariance-level summaries reflect net variance inflation but do not capture detailed nonlinear signatures (Section 4).

3.6.2. Energy Deviation and Failure Thresholds

To quantify DoS severity in an implementation-relevant manner, we characterize degradation using the trace-based energy deviation observable
Δ E DoS ∝ Tr ( V ′ ) − Tr ( V 0 ) ,
where V 0 denotes the covariance matrix of the unperturbed reference state. As excess variance accumulates, Δ E DoS grows rapidly, reflecting both increased quadrature variance and loss of state structure. Because Δ E is trace-based, it provides a rotation-invariant severity coordinate for variance/energy inflation, complementing rotation-sensitive signatures such as off-diagonal covariance growth, anisotropy metrics, or eigenvalue spread.
Operational failure occurs once the energy deviation exceeds a system-dependent threshold Δ E th , determined by detector dynamic range, estimator breakdown, numerical instability, control loop limits, or loss of protocol validity:
Δ E DoS ≫ Δ E th .
Crossing this threshold marks a transition from degraded performance to functional failure, beyond which meaningful CVQC operation cannot be maintained. Equivalently, in tolerance language (Section 3.1.1), DoS corresponds to Δ E and/or monitored covariance statistics, leaving their acceptance regions with near-unit detection probability over a single monitoring window, rather than requiring long-horizon accumulation. This is the “hard” end of the same finite-n visibility continuum used to define reconnaissance/exploration boundaries: while reconnaissance can have high P miss ( ν ) for typical n, DoS corresponds to disturbance levels for which P miss ( ν ) ≈ 0 over a single window.

3.6.3. Observability and Operational Consequences

Because DoS disturbances produce large-amplitude and rapidly varying deviations in quadrature statistics, they are typically straightforward to distinguish from lower-intensity regimes. The defining operational characteristic of DoS interference is speed: rapid variance inflation can destabilize the system on timescales shorter than those required for detailed diagnosis or corrective action (e.g., abrupt growth of Tr ( V ^ ) , abrupt increases in estimator variance across windows, or immediate violation of receiver dynamic-range constraints).
From an operational perspective, DoS disturbances delineate the ultimate boundary of adversarial tolerance in continuous-variable quantum systems. They define the regime in which physical-layer interference directly translates into loss of functionality, underscoring the importance of characterizing failure thresholds and the pathways through which adversarial perturbations drive systems from degraded operation into complete breakdown. Within the regime ladder of Figure 2, DoS corresponds to excursions beyond the receiver-defined failure threshold, whereas exploratory behavior corresponds to near-boundary stress that remains below sustained breakdown.

3.7. Operational Signatures in Covariance Statistics

Adversarial disturbances affect continuous-variable quantum states in ways that depend on both their intensity and operational intent. While all adversarial strategies perturb the underlying phase space distribution, their receiver-observable impact on state energy, coherence, and purity differs systematically across reconnaissance, exploratory, and denial-of-service regimes. These effects determine the reliability and operational stability of continuous-variable quantum communication systems and devices.
Table 6 summarizes how different receiver-accessible observables map to estimators, dominant failure modes, and regime sensitivity under finite-sample and finite-resolution constraints. Here, “most sensitive regime” is meant operationally: it indicates where an observable is most informative for distinguishing sub-threshold behavior, near-boundary stress, or outright failure under the receiver’s tolerance design and window size (and, when relevant, correlation-limited effective sample size).
Table 6. Mapping between receiver-accessible observables, estimators, dominant failure modes, and adversarial regime sensitivity in continuous-variable quantum communication. The table emphasizes how finite-sample estimation and implementation constraints shape operational vulnerability across adversarial regimes.

3.7.1. Energy Deviation as an Operational Metric

To quantify the impact of adversarial disturbances in a manner compatible with experimental continuous-variable platforms, we characterize variance/energy inflation using an energy deviation metric derived from second-order quadrature moments. For a single-mode Gaussian state with covariance matrix V, the mean energy (up to a constant offset set by normalization) is proportional to the trace of the covariance matrix, a standard result in Gaussian quantum optics and continuous-variable quantum information [4]:
⟨ E ⟩ ∝ Tr ( V ) .
The energy deviation induced by a disturbance is therefore defined as
Δ E ∝ Tr ( V ′ ) − Tr ( V 0 ) ,
Δ E : = Tr ( V ′ ) − Tr ( V 0 ) 4 ,
where V 0 denotes the covariance matrix of the unperturbed reference state and V ′ that of the perturbed state. Here we use δ e to denote a receiver-defined energy deviation tolerance (a scalar analogue of δ V ), i.e., the maximum Δ E typically accepted as nominal over a monitoring window at the chosen confidence level, as determined by finite-sample uncertainty, detector resolution, and false-alarm design. Covariance matrices are expressed in normalized units where the vacuum variance of each quadrature is set to unity. The proportionality is understood to apply to zero-mean states or to covariance matrices computed after the subtraction of estimated first moments, so that Tr ( V ) captures excess variance due solely to disturbance-driven fluctuations rather than coherent displacement.
Normalization and Affine Relation
Under the shot-noise unit normalization where the vacuum covariance is V vac = I 2 m for an m-mode system, the total mean photon number satisfies the affine relation
⟨ N ^ ⟩ = ∑ k = 1 m ⟨ n ^ k ⟩ = Tr ( V ) + ∥ d ∥ 2 − 2 m 4 ,
where d : = ⟨ r ^ ⟩ is the displacement vector. For mean-subtracted statistics ( d = 0 ), ⟨ N ^ ⟩ = Tr ( V ) − 2 m / 4 , so Δ E is directly interpretable as a receiver-accessible excess photon number (excess-energy) proxy induced by disturbance-driven covariance inflation.
Scope and Delimitation
Because Tr ( V ) is invariant under ideal phase space rotations, Δ E quantifies variance/energy inflation (e.g., an additive contribution via Tr ( N ) in the effective Gaussian model) but is blind to pure rotations that preserve the symplectic spectrum. Therefore, rotation-dominant disturbances are characterized in this framework using the anisotropy and off-diagonal structure of V ^ (e.g., V ^ x p ) and related rotation-sensitive signatures, rather than Δ E alone. We also emphasize that Tr ( V ) and variance estimation laws are standard tools in Gaussian-CV modeling and statistics; the contribution here is their operational repurposing as monitoring-layer primitives that induce tolerance-defined stealth bands and regime boundaries under finite-n inference.
Energy deviation serves as a practical, protocol-agnostic metric because it directly captures disturbance-driven variance accumulation, estimator degradation, and proximity to operational failure thresholds. It applies across communication, verification, and sensing tasks in continuous-variable systems. Different classes of adversarial disturbances correspond to distinct regimes of energy deviation:
  • Reconnaissance disturbances. Low-amplitude disturbances produce only a small increase in Tr ( V ) , yielding Δ E values that typically remain within estimator confidence intervals. Although energetically subtle, such deviations can accumulate over time, biasing inferred system parameters and enabling information leakage without triggering conventional anomaly detection.
  • Exploratory disturbances. Moderate, structured disturbances lead to observable increases in Δ E as quadrature variances become asymmetric or inflated. These deviations are constrained below catastrophic levels, allowing for repeated observation of system behavior while revealing sensitivity to controlled stress.
  • Denial-of-service (DoS) disturbances. High-intensity disturbances cause a rapid and large increase in Tr ( V ) , driving Δ E well beyond operational thresholds. In this regime, variance/energy growth correlates with estimator breakdown, detector saturation, and loss of functional viability.

3.7.2. Coherence Loss and State Purity

Beyond energy deviation, adversarial disturbances degrade quantum coherence and state purity, both of which are critical for reliable quantum information processing. These effects are naturally visualized in phase space via the Wigner function and quantified through changes in the covariance matrix.
  • Reconnaissance disturbances. Because reconnaissance disturbances remain energetically small, the Wigner function retains an approximately Gaussian and localized form over short timescales, and state purity is largely preserved. However, repeated low-level perturbations can accumulate, gradually degrading coherence and revealing information about system parameters without overt disruption.
  • Exploratory disturbances. Exploratory disturbances distort the covariance matrix more noticeably, producing elongation, rotation, or anisotropic spreading of the Wigner function in phase space. This reflects partial loss of coherence and moderate purity degradation, indicating proximity to stability boundaries.
  • Denial-of-service (DoS) disturbances. Under DoS conditions, large disturbances rapidly spread the Wigner function, yielding a highly mixed state with severely reduced purity. Nonclassical correlations and phase-sensitive structure are destroyed, rendering the quantum state unsuitable for communication, verification, or further processing.
From an operational perspective, these regimes define a structured progression of state degradation: from subtle parameter biasing, to stress-induced instability, to functional breakdown.
In multi-mode CVQC, mode coupling and shared references (e.g., common LO phase, shared calibration loops, or multiplexed channels) can induce inter-mode correlations that appear as off-diagonal blocks in V. Adversarial disturbances that are correlated across modes can therefore degrade performance without producing large per-mode variance inflation, particularly if they are engineered to concentrate in a low-dimensional subspace of the 2 m -dimensional phase space. Operationally, this motivates monitoring not only Tr ( V ) but also cross-covariances between modes, since inter-mode targeting can manifest primarily through growth of cross-terms rather than diagonal variances. These considerations do not change the regime taxonomy (recon/explor/DoS), but they expand the set of receiver-observable signatures that delineate regime transitions in multi-mode operation.

3.7.3. Normalization and Multi-Mode Generalization

Throughout this work, covariance matrices are expressed in normalized units where the vacuum variance of each quadrature is set to unity. This convention is standard in continuous-variable quantum optics and simplifies comparison across devices, protocols, and operating regimes by eliminating system-dependent scaling factors. Under this normalization, effective excess noise parameters, estimator tolerances, and energy deviation can be interpreted directly in terms of deviations from the vacuum reference, without explicit dependence on absolute optical power or Hamiltonian parameters.
The energy deviation metric introduced in this paper inherits this normalization naturally. For a single-mode Gaussian state with covariance matrix V, the quantity Tr ( V ) provides a dimensionless measure of total quadrature variance relative to vacuum. As a result, energy deviation captures disturbance-driven variance accumulation in a manner that is both experimentally accessible and independent of specific detector calibrations, provided consistent normalization is maintained.
Although the analysis presented here focuses primarily on single-mode qumodes for clarity, the framework extends to multi-mode continuous-variable systems. For an m-mode Gaussian state with covariance matrix V ∈ R 2 m × 2 m , the total energy deviation generalizes to
Δ E ∝ Tr ( V ′ ) − Tr ( V 0 ) ,
where V 0 denotes the reference covariance matrix of the unperturbed multi-mode state.

3.7.4. Why the Covariance Trace

A central design choice in this work is the use of the trace of the covariance matrix as the primary scalar observable for quantifying adversarial impact. This choice is motivated by physical relevance, experimental accessibility, and robustness under implementation constraints.
First, for Gaussian continuous-variable states, the trace of the covariance matrix
Tr ( V ) = ∑ k = 1 m ( ⟨ Δ x ^ k 2 ⟩ + ⟨ Δ p ^ k 2 ⟩ ) ,
is directly proportional (up to a constant offset set by normalization) to the mean energy or mean photon number for mean-subtracted statistics. As such, increases in Tr ( V ) provide a physically meaningful measure of disturbance-driven variance accumulation that is independent of phase space orientation.
Second, the trace is invariant under ideal symplectic rotations. This invariance is useful in adversarial settings, where structured disturbances may project differently onto measured quadratures depending on phase space orientation. Orientation-dependent effects remain observable through the full covariance structure, but the trace provides a compact summary of overall disturbance severity.
Third, from an experimental standpoint, the trace depends only on second-order quadrature moments, which can be estimated using homodyne or heterodyne detection with finite-resolution and without full state tomography. In contrast, alternative quantities such as symplectic eigenvalues, entropic measures, or fidelity metrics typically require stronger assumptions, higher-order statistics, or substantially larger data sets, making them less suitable for real-time monitoring.
Finally, the covariance trace provides a protocol-agnostic link between adversarial interference and operational thresholds. Estimator breakdown, detector saturation, numerical instability, and protocol abort conditions are naturally associated with excessive variance growth rather than with specific geometric features of the state. By framing adversarial impact in terms of Tr ( V ) , the resulting energy deviation metric reflects proximity to such failure modes across communication, verification, and sensing applications.

3.8. Finite-Sample Detectability: A Minimal Quantitative Demonstration

Remark 3 
(Rotation invariance and additive noise contribution to the trace). Let R be any phase space rotation (i.e., an orthogonal symplectic matrix with R T R = I and R Ω R T = Ω ), and let N ⪰ 0 . Then Tr ( R V R T ) = Tr ( V ) and Tr ( V + N ) = Tr ( V ) + Tr ( N ) ≥ Tr ( V ) [27].
Moreover, for the effective receiver model V ′ = G V G T + N implied by Equation (1)
Tr ( V ′ ) = Tr ( G V G T ) + Tr ( N ) ,
so the covariance trace separates a strictly additive contribution from effective excess noise through Tr ( N ) . While Tr ( G V G T ) can vary with unknown gain/mixing G, Tr ( V ) remains invariant to unknown phase space rotations (captured by R). This makes Tr ( V ) a natural scalar observable for receiver-side monitoring under unknown phase reference and mechanism-agnostic adversarial behavior.
  • Scope and contribution of the finite-sample analysis
This section relies on standard finite-sample statistics (sample variance estimation, χ 2 quantiles, and large-n normal approximations). The contribution is therefore not the χ 2 law itself nor the fact that detectability scales as 1 / n , but the operationalization of detectability for adversarial interference in CVQC: tolerances are treated as explicit receiver-defined acceptance regions; missed-detection probability is computed as a function of an effective disturbance-driven excess variance increment and window size; and this induces a soft operational boundary separating reconnaissance (statistically hidden within tolerances) from exploration (statistically resolvable stress/bias).

3.8.1. Setup: Estimating Effective Excess Variance from Quadrature Samples

We provide a minimal quantitative demonstration of how finite-sample size and finite-resolution estimation induce an operational detectability threshold for weak adversarial disturbances. The goal is not to propose a complete detector or security proof, but to make explicit the statistical mechanism that underlies the reconnaissance/exploratory regime boundary: below a sample-limited threshold, a disturbance that manifests as an effective excess variance increment can be statistically indistinguishable from nominal operation at typical confidence requirements. This behavior mirrors finite-size parameter estimation effects analyzed in CV-QKD, where excess noise below an estimator confidence boundary remains operationally invisible with nonzero probability despite being systematic [5,6,7]. Importantly, the qualitative regime structure discussed below does not depend on the normal approximation itself; the same 1 / n scaling and soft boundary follow from the exact χ 2 distribution.
Consider a receiver performing homodyne measurements of a single quadrature (without loss of generality, the p-quadrature) on n independent state preparations. Let { p i } i = 1 n denote the recorded outcomes. Under nominal operation, assume a zero-mean Gaussian model
p i ∼ N ( 0 , σ 0 2 ) ,
where σ 0 2 represents the reference quadrature variance, including trusted receiver noise contributions. Under adversarial disturbance, the receiver-observed variance becomes
σ 1 2 = σ 0 2 + ν ,
where ν ≥ 0 denotes the effective excess variance increment induced by the disturbance in the monitored quadrature.
A natural estimator for the quadrature variance is the sample variance
σ ^ 2 : = 1 n ∑ i = 1 n p i 2 ,
where the mean is taken to be 0 for simplicity, consistent with symmetric modulation or calibrated offset removal. More generally, the standard estimator 1 n ∑ i = 1 n ( p i − p ¯ ) 2 yields the same scaling of estimator uncertainty with sample size, and the zero-mean form is adopted here for notational clarity. For Gaussian samples, σ ^ 2 is an unbiased estimator with
E [ σ ^ 2 ] = σ 2 ,   Var ( σ ^ 2 ) = 2 σ 4 n .
Thus, under nominal operation ( σ 2 = σ 0 2 ), the standard deviation of the variance estimator scales as
Std ( σ ^ 2 ) = 2 n   σ 0 2 .
To connect to operational acceptance regions, suppose the receiver uses a one-sided threshold test of the form
σ ^ 2 ≤ σ 0 2 + τ ,
where τ encodes an estimator tolerance determined by the target false-alarm probability (confidence level), finite-resolution effects, and additional trusted uncertainty margins. When emphasizing this dependence we write τ ≡ τ α .
  • Exact finite-sample distribution (Gaussian case)
For Gaussian quadrature samples p i ∼ N ( 0 , σ 2 ) with known (or pre-subtracted) mean, the variance estimator σ ^ 2 = 1 n ∑ i = 1 n p i 2 admits the exact finite-sample law
n   σ ^ 2 σ 2 ∼ χ n 2 .
If instead one uses the usual sample-mean-corrected estimator s 2 = 1 n − 1 ∑ i = 1 n ( p i − p ¯ ) 2 , then
( n − 1 )   s 2 σ 2 ∼ χ n − 1 2 .
In what follows, we use a normal (Gaussian) approximation to this χ 2 -based sampling distribution in the large-n regime to obtain a simple closed-form scaling rule.
  • Correlation-aware interpretation
The derivations above assume i.i.d. samples within a monitoring window and stationary tolerances over that window. In deployed links, temporal correlations (e.g., phase reference dynamics, drift, and control loops) reduce statistical resolution relative to the nominal n. A standard proxy is an effective sample size n eff ≤ n , which (to leading order) widens the detectability scale by the substitution n ↦ n eff . A quantitative sensitivity discussion and an AR(1) illustration are given in Section 3.8.5.
In the large-n regime, a normal approximation yields a baseline operational detectability condition:
ν ≳ z 1 − α 2 n   σ 0 2 ,
where z 1 − α is the one-sided normal quantile associated with the desired significance level α . Equation (31) makes explicit the finite-sample scaling: the minimum effective excess variance that can be reliably resolved decreases only as 1 / n and grows with the baseline variance scale σ 0 2 .
This scaling underpins the operational interpretation adopted throughout the paper: reconnaissance corresponds to ν values below (or comparable to) the finite-sample detectability scale in Equation (31) over typical monitoring windows, while exploration corresponds to ν values that exceed it and therefore produce statistically resolvable distortions in receiver-side covariance statistics.
Numerical illustration (order-of-magnitude). To make the reconnaissance/exploratory boundary concrete, consider vacuum-normalized operation with σ 0 2 = 1 (shot-noise units) and a one-sided significance level α = 10 − 2 (so z 1 − α ≃ 2.33 ). Then Equation (31) yields the detectability scale shown in Table 7:
Table 7. Finite-sample detectability scale for effective excess variance (vacuum-normalized σ 0 2 = 1 , one-sided α = 10 − 2 ). Values show the order of magnitude of ν required for statistically reliable resolution under variance monitoring.

3.8.2. Tolerance Regions and Missed-Detection Probability

We now make explicit how estimator tolerances translate into a nonzero probability of missed-detection for weak adversarial disturbances.
Let the receiver adopt a variance-based acceptance test of the form
σ ^ 2 ≤ σ 0 2 + τ ,
where σ 0 2 is the reference variance under nominal operation and τ > 0 defines the tolerance margin.
Under disturbance, the true variance is σ 1 2 = σ 0 2 + ν . The probability of missed-detection (Type-II error) is therefore
P miss ( ν ) = Pr   σ ^ 2 ≤ σ 0 2 + τ   |   σ 2 = σ 0 2 + ν .
Using the Gaussian approximation for the sampling distribution of σ ^ 2 in the large-n regime
σ ^ 2 ∼ N   σ 1 2 ,   2 σ 1 4 n ,
the missed-detection probability can be written explicitly as
P miss ( ν ) = Φ   τ − ν 2   σ 1 2 / n ,
where Φ ( · ) denotes the cumulative distribution function of the standard normal distribution.
Equation (35) makes several operational features explicit. For ν ≪ τ , one obtains P miss ≈ 1 : disturbance-induced excess variance is almost certainly accepted as nominal. The transition from high to low missed-detection probability occurs over a finite interval of ν whose width scales as σ 1 2 / n , defining a soft detectability boundary rather than a sharp threshold.
  • Companion operational metrics
The same tolerance rule induces a false-alarm probability (Type-I error)
P FA = Pr   σ ^ 2 > σ 0 2 + τ   |   σ 2 = σ 0 2 = 1 − Φ   τ 2   σ 0 2 / n ,
and the detection probability (power) is P det ( ν ) = 1 − P miss ( ν ) . Together, ( P FA , P det ) define a receiver operating characteristic (ROC) for variance-based monitoring, making the sensitivity/false-alarm trade-off explicit.

3.8.3. Operational Boundary Between Reconnaissance and Exploratory Regimes

Using P miss ( ν ) , an operational boundary can be defined by selecting a reference target P miss * ∈ ( 0 , 1 ) and solving P miss ( ν * ) = P miss * .

3.8.4. Monte Carlo Validation of the Missed-Detection Curve

To move beyond a purely illustrative numerical evaluation, we include a minimal Monte Carlo validation under the same stated baseline assumptions (i.i.d. Gaussian quadrature samples within a window and the one-sided tolerance test in Equation (32)). Monte Carlo estimates of P miss ( ν ) are obtained by simulating many independent blocks of length n, computing σ ^ 2 for each block, and estimating the acceptance frequency. The resulting points overlay the analytic prediction in Equation (35) and corroborate the finite-n soft boundary behavior.
In addition to the large-n normal approximation used for the closed-form expression in Equation (35), we also evaluate P miss ( ν ) using the exact χ 2 sampling law for the variance estimator (Equation (29)). Figure 5 overlays Monte Carlo estimates on both the exact and approximate curves; the normal approximation is accurate for large n, while the exact χ 2 curve provides a finite-n baseline.
Figure 5. Missed-detection probability P miss ( ν ) versus excess variance amplitude ν for multiple block sizes n at tolerance τ α ( σ 0 2 = 1 , one-sided α = 0.01 ). Solid curves: Exact finite-sample prediction from the χ 2 law (Equation (29)) evaluated under the one-sided acceptance test (Equation (32)). Dashed curves: Large-n normal approximation (Equation (35)). Markers: Monte Carlo estimates of P miss ( ν ) from i.i.d. Gaussian blocks evaluated under the same acceptance test; error bars denote ± 1 standard error. Monte Carlo blocks are generated under the same i.i.d. Gaussian baseline; this validates the finite-sample formula (sampling law + test), not a device-specific channel model.
Solving explicitly for the boundary amplitude ν * yields
ν * = τ − 2   ( σ 0 2 + ν * )   Φ − 1 ( P miss * ) n ,
where Φ − 1 ( · ) is the inverse standard normal cumulative distribution function.
Equation (37) is linear in ν ⋆ and admits an explicit solution. Define
k   : =   2 n   Φ − 1   P miss ⋆ .
Then (37) rearranges to
ν ⋆   =   τ − k   σ 0 2 1 + k .
Worked numerical example. As an illustrative parameterization in shot-noise units, let σ 0 2 = 1 , n = 10 6 , and choose a one-sided false-alarm level α = 0.01 (so z 1 − α ≈ 2.33 and τ α ≈ z 1 − α 2 / n   σ 0 2 ≈ 3.29 × 10 − 3 under the large-n approximation). For a target missed-detection probability P miss ⋆ = 0.05 , we have Φ − 1 ( 0.05 ) ≈ − 1.645 , so k ≈ − 2.33 × 10 − 3 , and (39) yields ν ⋆ ≈ 5.63 × 10 − 3 .
Equation (37) therefore defines a finite-sample operational boundary between adversarial regimes:
  • For ν ≪ ν * , P miss ≈ 1 and disturbance-induced excess variance is statistically indistinguishable from nominal fluctuations over the observation window (reconnaissance).
  • For ν ≳ ν * , P miss decreases appreciably and excess variance becomes intermittently or consistently observable (exploration).

3.8.5. Sensitivity to Temporal Correlations via an Effective Sample Size

To quantify the impact of non-i.i.d. sampling on the detectability boundary, one can introduce an effective sample size
n eff   : =   n 1 + 2 ∑ k = 1 n − 1 1 − k n ρ ( k ) ,
where ρ ( k ) is the lag-k autocorrelation of the monitored quadrature within the window. When correlations decay sufficiently fast, n eff ≈ n /   1 + 2 ∑ k ≥ 1 ρ ( k ) , and the leading-order effect is the substitution n ↦ n eff in 1 / n scaling. For an AR(1) model with ρ ( k ) = ϕ k ( | ϕ | < 1 ), the large-n approximation yields
n eff   ≈   n   1 − ϕ 1 + ϕ ,
so ϕ = 0.9 implies n eff ≈ 0.0526   n and an uncertainty inflation factor of n / n eff ≈ 4.36 relative to the i.i.d. baseline. This widens the tolerance-induced stealth band and shifts ν ⋆ upward for a fixed nominal window length.

3.8.6. Receiver-Side Monitoring Workflow (Illustrative)

To keep the scope descriptive, the taxonomy and finite-n boundary can be instantiated as a lightweight receiver-side monitoring-layer that interfaces with standard parameter estimation pipelines. For a chosen window size n and reference operating point V 0 , the receiver computes V ^ t per window, forms Δ E t : = Tr ( V ^ t ) − Tr ( V 0 ) / 4 (Equation (18)), and compares (i) tolerance-based acceptance tests at false-alarm level α and (ii) a detectability boundary ν ⋆ computed from (39) for a chosen P miss ⋆ . The mapping between ν and Δ E is model-dependent (e.g., Δ E = ν / 4 for the quadrature-biased illustration, Δ E = ν / 2 for isotropic V ′ = V 0 + ν I 2 ), so any Δ E -based boundary should state the monitored model explicitly. Algorithm 1 summarizes an illustrative receiver-side monitoring workflow implementing this receiver-side classification logic.
Algorithm 1 Receiver-side monitoring for regime classification (illustrative).
Require: 
Window size n, reference covariance V 0 , false-alarm level α , target P miss ⋆ , DoS threshold Δ E DoS (Equation (18) convention).
  1:
for each time window t do
  2:
      Acquire samples and compute V ^ t .
  3:
      Compute Δ E t ← Tr ( V ^ t ) − Tr ( V 0 ) / 4 .
  4:
      Compute tolerance τ α (exact χ 2 form or large-n approximation).
  5:
      Compute reconnaissance boundary ν * via (39).
  6:
      if Δ E t ≥ Δ E DoS then
  7:
           classify as DoS.
  8:
     else if Δ E t exceeds the detectability-scaled boundary for the monitored model (e.g., Δ E t ≳ ν * / 4 in the quadrature-biased example) then
  9:
           classify as exploration.
10:
     else
11:
           classify as reconnaissance.
12:
     end if
13:
     log/alert according to the operational policy.
14:
end for

4. Limitations and Scope

The framework developed in this work is intentionally scoped to operational characterization rather than mitigation or defense. Several limitations therefore delineate the regime of validity and interpretation of the results.
(1)
Observable scope: covariance-level monitoring.
The analysis is restricted to receiver-side observables, primarily first- and second-order quadrature statistics summarized by covariance matrices. While this choice reflects what is experimentally accessible in most continuous-variable quantum communication (CVQC) platforms, it does not capture higher-order moments, non-Gaussian features, or full state-tomographic information. Adversarial strategies whose distinguishing signatures reside mainly in higher-order structure (e.g., heavy tails, multimodality, non-Gaussian leakage) may therefore evade characterization within the present framework. We emphasize that this restriction is a deliberate modeling choice (receiver-observable instantiation) rather than a claim of completeness; the regime taxonomy is operational and can be instantiated with richer feature sets when such observables are available.
(2)
Phenomenological disturbance modeling at the level of observables.
The modeling of adversarial disturbances is phenomenological and Gaussian at the level of receiver-observed statistics. This does not imply that adversaries are limited to Gaussian physical processes; rather, their impact is analyzed through the lens of finite-resolution estimation of covariance-level quantities. Non-Gaussian attacks that nonetheless manifest as effective excess variance (or effective covariance deformation) at the receiver are captured by the framework, whereas attacks whose signatures lie entirely outside covariance-level statistics are not. Therefore, covariance-only monitoring may miss higher-order and non-Gaussian signatures, even when the operational impact is significant.
(3)
Estimator space effectiveness versus physical realizability of ( G , N ) .
Equation (1) is used as an estimator space effective model: ( G , N ) summarizes how receiver-estimated first/second moments behave under finite-resolution inference. Therefore, unconstrained fitted ( G , N ) may represent calibration/interface distortions or aggregation effects that are not themselves physically realizable Gaussian quantum channels. If physical attribution is required, one can constrain or project ( G ^ , N ^ ) onto the physically realizable Gaussian channel feasibility set via standard complete-positivity constraints (as noted in Section 3). The present work does not enforce this because its goal is regime classification and visibility analysis, not mechanism identification.
(4)
Baseline assumptions in finite-sample detectability.
The finite-sample detectability analysis assumes independent and identically distributed quadrature samples and stationary estimator tolerances over each observation window. In realistic systems, temporal correlations, drifting calibration parameters, non-stationary channels, or adaptive monitoring strategies may modify detectability boundaries and acceptance regions. The results should therefore be interpreted as baseline operational limits and scaling laws rather than exhaustive detection guarantees. Section 3.8.5 introduces an effective sample size n eff ≤ n and shows how temporal correlation inflates uncertainty and shifts ν ⋆ through the substitution n ↦ n eff , widening tolerance-induced stealth bands relative to the i.i.d. baseline.
(5)
Relationship to protocol-level security proofs.
In CV-QKD and related security proof frameworks, finite-size parameter estimation error refers to statistical fluctuation of an estimator around its nominal value (confidence regions), whereas adversarial parameter bias refers to systematic, potentially non-stationary manipulation that shifts the underlying effective channel parameters. Composable security analyses typically absorb stationary excess noise into worst-case bounds under explicit modeling assumptions (often collective/i.i.d. structure together with reduction arguments). In contrast, the adversarial regimes emphasized here explicitly include estimator-targeting and time-structured disturbances whose operational effect is to shape what the receiver infers within tolerance regions. Therefore, the present work should be read as a receiver-observable operational threat model complementary to (and not replacing) protocol-level security proofs.
Moreover, many CV-QKD composable security reductions rely on permutation invariance and collective/i.i.d.-style modeling assumptions. Time-correlated, non-stationary, or estimator-targeting disturbances can violate these assumptions, so translating the present regime taxonomy into protocol-level security bounds requires additional modeling beyond covariance-only characterization.
(6)
Single-mode focus and deployment scope.
The work focuses on single-mode states and single-link communication scenarios. While the covariance trace and energy deviation concepts generalize naturally to multi-mode systems, correlated noise, mode coupling, shared references, and network-level effects are not explicitly analyzed here. Extending the framework to multi-mode and networked settings is therefore necessary for full-scale deployment scenarios.
(7)
No concrete countermeasures or optimal monitoring design.
This paper does not propose concrete countermeasures, adaptive controls, or protocol-level defenses. While the taxonomy and quantitative boundaries introduced here are intended to inform such strategies, their design and validation lie outside the scope of the present study. In particular, questions of optimal monitoring, adaptive thresholding, feedback control, and integration with quantum error correction, verification, or protocol abort logic are deferred to future work.
Within these bounds, the contribution of this paper is to provide a clear operational lens through which adversarial interference in CVQC can be classified, quantified, and compared. The scope is complementary to work on mitigation, control, and security proofs, supplying a receiver-centric threat modeling substrate upon which such defenses can be evaluated.

5. Conclusions

This work developed an operational framework for characterizing adversarial interference in continuous-variable quantum communication (CVQC) under implementation-realistic constraints, including finite measurement resolution, estimator tolerances, finite-sample sizes, and limited control capabilities. Rather than treating noise as purely environmental and stationary, adversarial interference was modeled as structured, intent-driven disturbances that can be engineered to remain operationally inconspicuous, probe system stability, or rapidly disrupt functionality.
Within a receiver-side Gaussian channel representation, we introduced a three-regime taxonomy of adversarial disturbances. Reconnaissance disturbances consist of low-amplitude perturbations designed to evade detection while gradually biasing parameter estimation within tolerance regions. Exploratory disturbances introduce moderate, structured perturbations that induce observable stress and intermittently resolvable deviations, revealing directional sensitivities and stability margins without forcing immediate failure. Denial-of-service (DoS) disturbances correspond to high-intensity interference that overwhelms the system, driving rapid loss of state integrity and operational breakdown. To quantify these regimes in a protocol-agnostic and experimentally accessible manner, we defined an energy deviation metric based on the covariance trace, Δ E ∝ Tr( V ^ ) − Tr ( V 0 ) , providing a compact scalar measure of excess variance accumulation and proximity to operational failure thresholds while remaining invariant under ideal phase space rotations.
A central message is that adversarial regimes are most meaningfully defined by their interaction with receiver estimation limits, not by idealized mechanism labels. Therefore, we operationalized finite-size observability by expressing estimator tolerances as receiver-defined acceptance regions and deriving explicit missed-detection and detectability scaling laws that connect disturbance amplitude, tolerance margins, and sample size. This analysis makes concrete the existence of an operational “blind band” in which systematic perturbations can remain statistically consistent with nominal operation over finite monitoring windows, thereby formalizing the soft boundary between reconnaissance and exploratory behavior.
Together, the proposed taxonomy, covariance trace metric, and finite-sample boundary analysis establish a structured threat modeling foundation for analyzing physical-layer attack surfaces in CVQC. By linking adversarial intent to receiver-accessible phase space statistics, the framework enables systematic comparison of how subtle perturbations can bias inference and accumulate degradation before escalating into destabilizing interference. More broadly, it provides a common operational language connecting physical-layer disturbances to estimator degradation, coherence/purity loss, and system-level performance limits across communication, verification, and sensing settings.
To complement the schematic regime illustrations, the manuscript includes Monte Carlo simulation overlays of the missed-detection probability P miss ( ν ) versus ν for multiple window sizes n (Section 3.8). These plots corroborate the finite-n soft boundary behavior predicted by the χ 2 -based analysis under the stated i.i.d. baseline assumptions, and they illustrate how the reconnaissance/exploration transition sharpens with increasing n while remaining nontrivial for finite windows.
The framework developed here motivates future work focused on mitigation and resilience rather than characterization alone. Promising directions include extending the monitoring-layer beyond covariance-only statistics (e.g., higher-order and time-series tests), incorporating real-time feedback and adaptive thresholding, and generalizing to multi-mode and networked architectures where correlated disturbances may manifest primarily through cross-covariance structure. Integration with higher-level verification, error-correction, and protocol logic is also a natural next step toward resilient continuous-variable quantum communication and information-processing platforms.
From a methodology standpoint, future work on adversarial detection can draw on established statistical monitoring and change detection literature to test temporal and multi-observable consistency of receiver-side estimators under structured disturbances, including sequential detection and drift monitoring approaches [22,23]. This avoids relying on unrelated deep-learning/MANET intrusion-detection citations and provides a more appropriate monitoring-theoretic connection for the receiver-side setting.
For clarity, we summarize the manuscript’s core contributions as follows:
  • Mechanism-agnostic adversarial taxonomy. A receiver-centric classification of adversarial interference into reconnaissance, exploratory, and denial-of-service regimes, defined by observable impact relative to estimator tolerances rather than by assumed physical attack mechanisms.
  • Receiver-observable estimator space modeling. A phenomenological ( G , N ) framework capturing effective disturbance impact at the level of receiver-accessible covariance statistics, with an explicit discussion of non-identifiability and of physical plausibility constraints when mechanism attribution is required.
  • Finite-sample visibility and validation. Explicit missed-detection and detectability scaling laws linking effective excess variance amplitude, tolerance, and sample size, together with Monte Carlo validation plots that corroborate the predicted P miss ( ν ) behavior under the stated baseline assumptions.
Together, these contributions shift the emphasis from “how much noise breaks key rate” to “what classes of sub-threshold disturbances can remain operationally invisible under finite-n monitoring and how they escalate to failure,” applicable to CVQC beyond QKD.

Author Contributions

Conceptualization, J.R.R.-B.; methodology, J.R.R.-B. and J.V.G.T.; investigation, J.R.R.-B.; validation, J.V.G.T. and R.A.F.; formal analysis, J.R.R.-B.; writing—original draft, J.R.R.-B.; writing—review and editing, J.V.G.T., R.A.F., N.S., S.R.V., M.P., A.T. (Alexander Truskovsky) and A.T. (Andy Thanos); supervision, R.A.F. All authors have read and agreed to the published version of the manuscript.

Funding

This research study was funded in part by the Natural Sciences and Engineering Research Council of Canada (NSERC), Discovery Grants Program, Grant No. RGPIN-2023-04513, in association with Lakes Environmental Research Inc. and EigenQ, Inc. Cette recherche a été financée par le Conseil de recherches en sciences naturelles et en génie du Canada (CRSNG), RGPIN-2023-04513.

Institutional Review Board Statement

Not applicable.

Data Availability Statement

Data available from the corresponding author upon reasonable request.

Conflicts of Interest

Author Nadeem Said is an employee of LAKES Environmental Research Inc. Author Andy Thanos is an employee of Cisco Systems, Inc. Authors Jose R. Rosas-Bustos, Jesse Van Griensven The, Mark Pecen, Sebastian Ratto Valderrama, and Alexander Truskovsky are Consultants to EigenQ Inc. Roydon Andrew Fraser is a paid advisor to EigenQ Inc. The remaining authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Abbreviations

The following abbreviations are used in this manuscript:
ADCAnalog-to-Digital Converter
CUSUMCumulative Sum
CVContinuous-Variable
CVQCContinuous-Variable Quantum Communication
CV-QKDContinuous-Variable Quantum Key Distribution
DoSDenial-of-Service
LOLocal Oscillator
QIPQuantum Information Processing
QKDQuantum Key Distribution
ROCReceiver Operating Characteristic
SNUShot-Noise Unit
TTPTactics, Techniques, and Procedures

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