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Circular error probable
Circular error probable
from Wikipedia
CEP concept and hit probability. 0.2% outside the outmost circle.

Circular error probable (CEP),[1] also circular error probability[2] or circle of equal probability,[3] is a measure of a weapon system's precision in the military science of ballistics. It is defined as the radius of a circle, centered on the aimpoint, that is expected to enclose the landing points of 50% of the rounds; said otherwise, it is the median error radius, which is a 50% confidence interval.[1][4] That is, if a given munitions design has a CEP of 10 m, when 100 munitions are targeted at the same point, an average of 50 will fall within a circle with a radius of 10 m about that point.

An associated concept, the DRMS (distance root mean square), calculates the square root of the average squared distance error, a form of the standard deviation. Another is the R95, which is the radius of the circle where 95% of the values would fall, a 95% confidence interval.

The concept of CEP also plays a role when measuring the accuracy of a position obtained by a navigation system, such as GPS or older systems such as LORAN and Loran-C.

Concept

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Circular bivariate normal distribution
20 hits distribution example

The original concept of CEP was based on a circular bivariate normal distribution (CBN) with CEP as a parameter of the CBN just as μ and σ are parameters of the normal distribution. Munitions with this distribution behavior tend to cluster around the mean impact point, with most reasonably close, progressively fewer and fewer further away, and very few at long distance. That is, if CEP is n metres, 50% of shots land within n metres of the mean impact, 43.7% between n and 2n, and 6.1% between 2n and 3n metres, and the proportion of shots that land farther than three times the CEP from the mean is only 0.2%.

CEP is not a good measure of accuracy when this distribution behavior is not met. Munitions may also have larger standard deviation of range errors than the standard deviation of azimuth (deflection) errors, resulting in an elliptical confidence region. Munition samples may not be exactly on target, that is, the mean vector will not be (0,0). This is referred to as bias.

To incorporate accuracy into the CEP concept in these conditions, CEP can be defined as the square root of the mean square error (MSE). The MSE will be the sum of the variance of the range error plus the variance of the azimuth error plus the covariance of the range error with the azimuth error plus the square of the bias. Thus the MSE results from pooling all these sources of error, geometrically corresponding to radius of a circle within which 50% of rounds will land.

Several methods have been introduced to estimate CEP from shot data. Included in these methods are the plug-in approach of Blischke and Halpin (1966), the Bayesian approach of Spall and Maryak (1992), and the maximum likelihood approach of Winkler and Bickert (2012). The Spall and Maryak approach applies when the shot data represent a mixture of different projectile characteristics (e.g., shots from multiple munitions types or from multiple locations directed at one target).

Conversion

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While 50% is a very common definition for CEP, the circle dimension can be defined for percentages. Percentiles can be determined by recognizing that the horizontal position error is defined by a 2D vector which components are two orthogonal Gaussian random variables (one for each axis), assumed uncorrelated, each having a standard deviation . The distance error is the magnitude of that vector; it is a property of 2D Gaussian vectors that the magnitude follows the Rayleigh distribution, with scale factor . The distance root mean square (DRMS), is and doubles as a sort of standard deviation, since errors within this value make up 63% of the sample represented by the bivariate circular distribution. In turn, the properties of the Rayleigh distribution are that its percentile at level is given by the following formula:

or, expressed in terms of the DRMS:

The relation between and are given by the following table, where the values for DRMS and 2DRMS (twice the distance root mean square) are specific to the Rayleigh distribution and are found numerically, while the CEP, R95 (95% radius) and R99.7 (99.7% radius) values are defined based on the 68–95–99.7 rule:

Measure of Probability
DRMS 63.213...
CEP 50
2DRMS 98.169...
R95 95
R99.7 99.7

We can then derive a conversion table to convert values expressed for one percentile level, to another.[5][6] Said conversion table, giving the coefficients to convert into , is given by:

From to RMS () CEP DRMS R95 2DRMS R99.7
RMS () 1.00 1.18 1.41 2.45 2.83 3.41
CEP 0.849 1.00 1.20 2.08 2.40 2.90
DRMS 0.707 0.833 1.00 1.73 2.00 2.41
R95 0.409 0.481 0.578 1.00 1.16 1.39
2DRMS 0.354 0.416 0.500 0.865 1.00 1.21
R99.7 0.293 0.345 0.415 0.718 0.830 1.00

For example, a GPS receiver having a 1.25 m DRMS will have a 1.25 m × 1.73 = 2.16 m 95% radius.

See also

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References

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Further reading

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Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
Circular error probable (CEP) is a statistical measure of accuracy for delivery systems in , defined as the of a centered on the aim point within which half of the projectiles or impacts are expected to land. This metric serves as an indicator of a system's precision and is used to evaluate probable damage to targets when direct observation is unavailable. CEP assumes that errors in the range and deflection directions (both in the horizontal plane) follow independent Gaussian distributions, leading to a for the radial error distance. In practice, for circularly symmetric errors where the standard deviations in both directions are equal (σ_x = σ_y = σ), the CEP is calculated as approximately 1.1774σ, derived from the inverse of the Rayleigh at the 50% probability level. For noncircular cases (σ_x ≠ σ_y), approximations adjust for the differing variances using the root-sum-square error and a correction factor based on the chi-square distribution, ensuring the circle encloses 50% of impacts with minimal error (typically under 2%). This makes CEP a practical tool for comparing weapon systems, such as missiles or , where lower values indicate higher accuracy. Beyond military applications, CEP is also employed in and positioning systems, including (GPS) receivers, to describe horizontal accuracy as the radius containing 50% of position fixes relative to the true location. In these contexts, it complements other metrics like error (RMS) but focuses specifically on the probabilistic containment in a circular area, aiding in assessments for , , and autonomous systems.

Definition and Fundamentals

Core Definition

Circular error probable (CEP) is a probabilistic measure of accuracy in two-dimensional targeting or positioning systems, defined as the radius of a circle centered on the target point (or aim point) that is expected to enclose 50% of the impacts or measurement errors from a set of shots or observations. This metric quantifies the precision of systems such as munitions, navigation devices, or sensors by focusing on the central tendency of error dispersion in a plane. The 50% probability threshold in CEP corresponds to the radial , interpreting the value as the distance within which half of all errors occur, providing a robust indicator of typical performance that is less sensitive to outliers than mean-based measures. Under standard statistical assumptions, such as those involving a bivariate for error coordinates, this radius captures the core spread of impacts around the intended point. For instance, in testing, a CEP of 100 meters means that approximately half of the warheads from multiple launches would land within a 100-meter radius of the designated aim point, aiding evaluators in assessing system reliability without requiring exhaustive data on every shot. This approach simplifies the communication of accuracy for military and engineering applications. CEP was first formalized in the mid-20th century as a tool for evaluating bombing accuracy, with early applications during where bomber precision was measured in feet using this metric—for example, an average CEP of 1,200 feet in 1943.

Underlying Assumptions

The circular error probable (CEP) metric is predicated on the assumption that the errors in the crossrange (x) and downrange (y) directions are independent and follow normal distributions, collectively forming a bivariate for the impact points. This bivariate normality arises from the , as the cumulative effects of multiple independent random variables—such as guidance, atmospheric, and launch perturbations—tend toward a Gaussian form. Independence between the x and y components, typically indicated by a of zero, is essential for the validity of this model, ensuring that deviations in one direction do not influence the other. A key requirement for CEP is circular symmetry in the error distribution, which implies equal variances (and thus equal standard deviations) in the x and y directions. This symmetry results in a radially uniform probability density around the center, akin to the as a special case of the bivariate normal when the is at the origin and is absent. Without this equal-variance condition, the distribution becomes elliptical, complicating the direct application of standard CEP formulas and requiring adjustments for ellipticity. CEP assumes that individual shots or measurements are independent, with errors drawn from the same underlying distribution without autocorrelation or clustering effects. Moreover, it exclusively models random errors, necessitating the prior correction or removal of any systematic biases, such as consistent guidance offsets or environmental drifts, to isolate the component. Failure to address these biases can inflate the apparent CEP, as they shift the entire distribution away from the intended center. The target point serves as the true of the error distribution, positioned at the origin (0,0) after bias corrections, ensuring that the CEP encapsulates the probabilistic spread around this central aim. This centering aligns with the metric's focus on random dispersion relative to the expected impact location.

Historical Development

Origins in

The circular error probable (CEP), defined as the radius of a circle centered on the aim point expected to enclose 50% of bomb impacts, emerged during as a key metric for quantifying the accuracy of aerial bombing conducted by Allied forces against German targets. Operations research teams analyzed bomb impact data from these campaigns to measure dispersion patterns, deriving CEP from statistical analysis of bomb dispersion patterns assuming bivariate normal distributions, providing a practical way to evaluate the effectiveness of unguided munitions under combat conditions. This approach was particularly vital for assessing the performance of systems like the , which in prewar tests achieved a CEP of approximately 150 feet (46 meters), though actual wartime results were significantly poorer due to factors such as weather and flak. Initial CEP calculations relied heavily on empirical data gathered from range tests and operational bombing runs, allowing analysts to derive accuracy estimates without relying on advanced statistical models that would come later. These methods involved plotting impact points from repeated firings or drops to determine the 50% containment radius, offering a straightforward tool for experts to compare weapon systems and refine targeting procedures. During the war, such evaluations highlighted the limitations of conventional bombing, with average CEPs of approximately 1,200 feet (366 meters) for high-altitude daylight raids in 1943. Following , the U.S. military formally adopted CEP in the 1950s as a standard for evaluating emerging guided munitions, building on wartime data to support the development of more precise and systems. This post-war integration marked a shift toward systematic accuracy assessments in munitions testing, with CEP becoming embedded in for ballistic applications.

Evolution in Modern Systems

During the , circular error probable (CEP) became a central metric in the testing and evaluation of intercontinental ballistic missiles (ICBMs) and submarine-launched ballistic missiles (SLBMs) by both the and the , spanning the 1960s to the 1980s. Advancements in guidance systems, such as inertial navigation improvements, enabled significant reductions in CEP values, transitioning from initial figures in the kilometers range during early deployments to hundreds of meters by the late period. For instance, U.S. Minuteman III ICBM upgrades in the 1970s reduced CEP from approximately 183 meters to 120 meters, enhancing targeting precision against hardened sites. Similarly, Soviet ICBM programs, including the SS-18 and SS-19 models, incorporated accuracy enhancements that lowered CEP to around 500 meters or better by the 1980s, as assessed in U.S. intelligence evaluations. These developments were integral to strategic deterrence testing at facilities like Vandenberg Air Force Base for the U.S. and for the USSR, where CEP served as a key performance indicator for warhead delivery reliability. Following the , the 1990s marked a pivotal shift in CEP application with the integration of (GPS) technology into munitions, dramatically improving accuracy in . This evolution was prominently demonstrated during the 1991 , where GPS- and laser-guided smart bombs achieved CEPs under 10 meters, a stark improvement over the roughly 100-meter CEPs of unguided munitions used in prior conflicts. The deployment of systems like the laser-guided bomb allowed coalition forces to precisely strike Iraqi targets, such as armored columns and command centers, with minimal compared to earlier dumb bomb deliveries. This incorporation of satellite navigation not only refined CEP as a benchmark for precision-guided munitions but also set the stage for its broader adoption in post-Cold War military doctrines. By 2025, CEP remains a standard metric in the evaluation of systems within U.S. Department of Defense (DoD) assessments, reflecting ongoing refinements for high-speed, maneuverable platforms. DoD reports on programs like the and emphasize CEP to quantify terminal accuracy against time-sensitive targets, often targeting sub-10-meter performance despite atmospheric challenges. These evaluations, detailed in annual testing summaries and congressional briefings, underscore CEP's enduring role in verifying the operational viability of hypersonics amid global competition.

Mathematical Foundations

Bivariate Normal Distribution Model

The circular error probable (CEP) is fundamentally underpinned by a that treats impact errors in two dimensions as arising from a bivariate normal distribution. In this framework, the errors in the orthogonal directions—typically denoted as crossrange (x) and downrange (y)—are modeled as jointly normally distributed random variables with their mean vector centered at the target point, assumed to be the origin (0, 0) in the absence of . This centering reflects the ideal case where the expected impact location coincides with the aim point. The distribution is characterized by a 2×2 covariance matrix that captures the variances in the x and y directions (σ_x² and σ_y²) along with the covariance between them (σ_xy). This matrix encapsulates the spread and any linear dependence in the error components, allowing for elliptical contours of equal probability density. For scenarios exhibiting circular symmetry, such as isotropic error distributions common in certain ballistics applications, the model simplifies by assuming equal variances (σ_x = σ_y = σ), resulting in a rotationally invariant distribution where the probability contours form perfect circles. A key assumption in the standard CEP model is that the x and y errors are uncorrelated, corresponding to a ρ = 0 between the components. This independence simplifies the joint and aligns with empirical observations in many unbiased, symmetric systems, where crossrange and downrange deviations do not systematically influence each other. Under these conditions, the bivariate normal reduces to a product of two independent univariate normals when σ_x = σ_y. The 50% containment probability central to CEP is derived from the (CDF) of this joint bivariate , integrated over the disk of r centered at the mean. Specifically, the CDF evaluates the probability that the from the target (√(x² + y²)) is less than or equal to r, yielding the proportion of impacts expected within that circle. For the isotropic, uncorrelated case, this integral corresponds to the CDF of a , providing a direct probabilistic interpretation of the containment .

Calculation Formulas

The circular error probable (CEP) for a system modeled by a bivariate with equal standard deviations σ_x = σ_y = σ and no is derived from the of the radial error r. The cumulative probability that the radial error is less than or equal to r is given by the 0rrσ2exp(r22σ2)dr=1exp(r22σ2).\int_0^r \frac{r'}{\sigma^2} \exp\left( -\frac{r'^2}{2\sigma^2} \right) dr' = 1 - \exp\left( -\frac{r^2}{2\sigma^2} \right). Setting this equal to 0.5 for the 50% probability level and solving yields r=σ2ln(0.5)=σ2ln21.177σ,r = \sigma \sqrt{-2 \ln(0.5)} = \sigma \sqrt{2 \ln 2} \approx 1.177 \sigma,
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