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Meridian arc

A meridian arc is the curved segment of a —a line of constant —on the Earth's ellipsoidal surface between two points of differing geodetic latitudes, representing the shortest path along the meridian between those latitudes. In , its length is computed using integrals over the ellipsoid's parametric equations, such as S(\varphi) = a \int_0^\varphi \sqrt{1 - e^2 \sin^2 \theta} \, d\theta, where a is the semi-major axis and e is the . Historically, meridian arc measurements have been pivotal in determining the Earth's figure, beginning with ancient approximations and advancing through precise surveys in the 18th century. Expeditions led by Pierre Louis Maupertuis in Lapland (1736–1737) and Charles Marie de La Condamine in Peru (1735–1745) measured arcs near 66°N and the equator, respectively, to verify Isaac Newton's prediction of an oblate spheroid, revealing that a degree of latitude is longer at the poles than at the equator. Earlier efforts, such as Jean Picard's 1669–1671 arc near Paris, provided initial data for ellipsoidal modeling, while Giovanni Battista Riccioli's 17th-century work refined estimates of the Earth's flattening. These measurements contributed to the development of reference ellipsoids, essential for global coordinate systems and . In modern , meridian arc lengths are approximated via series expansions, such as Helmert's up to fourth order in the third flattening n: S(\varphi) \approx a \left[ \varphi + \frac{n^2 \sin 2\varphi}{2} + \frac{n^3 \sin 4\varphi}{4} - \frac{n^4 \sin 6\varphi}{512} \right], enabling accurate transformations in map projections like the Universal Transverse Mercator (UTM). The (1816–1855), spanning over 2,800 km from the to the , exemplifies 19th-century international efforts to link regional surveys into a unified global framework. Today, like GPS refines these arcs, supporting applications in , , and climate modeling.

Fundamentals

Definition

In and , a is the curve on the 's surface connecting two points of the same but different latitudes, forming a segment of a meridian line. This represents the shortest path along the meridian between those latitudes on an ellipsoidal model of the . While early approximations treated the as a for simplicity, modern employs an oblate ellipsoid of revolution to better capture the planet's caused by rotation. The spherical model introduces systematic errors in lengths—up to about 0.3% over a full —making the ellipsoidal approach essential for precise distance computations in , mapping, and global positioning systems. The is defined by parameters such as the semi-major axis a (equatorial ) and f = (a - b)/a, where b is the semi-minor axis (polar ). These determine the meridian's shape, with arc lengths varying nonlinearly with latitude differences. For the 1984 (WGS84) , a = 6378137 m and f = 1/298.257223563. As an illustration, the meridian arc from the (\phi = 0^\circ) to the (\phi = 90^\circ) measures approximately 10,002 km under WGS84.

Geometric Properties

The meridian arc represents the along the passing through the poles on an of revolution, which models the Earth's slightly shape. Positions along this arc are defined by various measures, each serving distinct geometric roles in . The geodetic \phi, also known as geographic , is the between the normal to the surface at a point and the equatorial plane; it is the standard used in and . The geocentric \psi is the between the line from the Earth's to the point and the equatorial plane, differing from \phi due to the ellipsoid's , with the relation \tan \psi = (1 - e^2) \tan \phi, where e is the first . The parametric \beta, or reduced , is an auxiliary facilitating representations, related by \tan \beta = \sqrt{1 - e^2} \tan \phi. In the meridional plane, the arc traces a on the , characterized by two principal . The in the prime vertical N(\phi), perpendicular to the , is given by N(\phi) = \frac{a}{\sqrt{1 - e^2 \sin^2 \phi}}, where a is the semi-major axis. The M(\phi), along the arc direction, is M(\phi) = \frac{a (1 - e^2)}{(1 - e^2 \sin^2 \phi)^{3/2}}. These radii vary with , being equal at the and poles but differing elsewhere, influencing local . The parametric equations for a point on the (in the x-z plane, with fixed at zero) express Cartesian coordinates in terms of geodetic : x = N(\phi) \cos \phi, \quad z = N(\phi) (1 - e^2) \sin \phi. Equivalently, using parametric \beta, the forms an : x = a \cos \beta, \quad z = b \sin \beta, where b = a (1 - f) is the semi-minor axis and f is the . This elliptical trace in the x-z plane visualizes the meridian arc as the generating curve of the of revolution, spanning from the (\phi = 0) to the (\phi = 90^\circ).

Historical Measurements

Pre-19th Century Efforts

Early efforts to measure the meridian arc date back to ancient times, with the Greek scholar providing the first reasonably accurate estimate around 240 BCE. Observing that the Sun was directly overhead at noon on the summer solstice in Syene (modern , ), while in it cast a shadow at an angle of 7.2 degrees (one-fiftieth of a full circle), used the known distance between the cities—approximately 5,000 , as reported by professional pacers (bematists)—to calculate the Earth's full circumference as 250,000 . This corresponded to an equatorial circumference of roughly 39,690 to 46,100 kilometers, depending on the exact length of the (estimated at 157 to 185 meters), remarkably close to the modern value of about 40,075 kilometers and implying a meridian arc length per degree of around 110 kilometers under a spherical assumption. In the , refined estimates of the Earth's flattening through comparisons of lengths and lunar observations, proposing a semi-minor axis about 1/270 shorter than the equatorial, influencing subsequent ellipsoidal modeling. More precise geodetic surveys emerged in , beginning with Jean Picard's measurement of a meridian arc near from 1669 to 1671. Picard employed , a method developed by , using a fitted with a for measurements and wooden rods to establish baselines with a precision of about 1 in 10,000; his arc spanned roughly 1 of latitude from to Sourdon (near ), yielding a length of 57,060 s for one . The , France's standard at the time—defined as approximately 1.949 meters and based on the distance of a person's outstretched arms—served as the baseline for these linear measurements, ensuring consistency in surveying across regions. Picard's result, equivalent to about 111.21 kilometers per , marked a significant improvement in accuracy and laid the foundation for national mapping efforts. The Cassini family extended Picard's work throughout the , creating one of the earliest comprehensive networks in . Starting in 1700 under (Cassini I) and continued by his son Jacques Cassini (Cassini II), the survey expanded the arc northward to and southward to the by 1718, and further to by around 1740, covering approximately 9.5 degrees or 1,000 kilometers. These extensions relied on similar techniques with improved instruments, such as larger sectors and theodolites, and confirmed a degree length averaging close to Picard's value but suggested a prolate (elongated) shape, contrary to Newton's oblate spheroid theory. Complementary observations, pioneered by in 1657 and notably by Jean Richer in 1672–1673 (who found pendulums required shortening by 2.82 millimeters near the in compared to ), helped quantify local gravity variations with latitude, providing indirect evidence for Earth's non-spherical form by linking period to . To resolve the debate between prolate and oblate models, the sponsored expeditions in the mid-18th century. led the Lapland expedition (1736–1737), measuring a ~1° meridian arc near 66°N from to Kittisvaara, yielding 57,437.9 toises (~111.9 km) per degree using and baseline measurements. Simultaneously, Charles Marie de La Condamine directed the Peruvian expedition (1735–1745) near , measuring a ~3° arc at the spanning 176,260 toises (~56.7 km per degree), despite challenges like terrain and political issues. These results demonstrated longer degrees at higher latitudes, confirming Newton's oblate spheroid and advancing ellipsoidal models. These pre-19th century measurements faced significant challenges stemming from the prevailing assumption of a perfectly , which overlooked the planet's oblateness and led to inconsistencies in arc lengths across latitudes. For instance, early calculations, including Newton's estimate of polar at 1/229, overestimated the actual value (modern 1/298.3) by treating meridians as perfect circles rather than ellipses, resulting in erroneous models like the Cassinis' prolate . Such assumptions complicated efforts to reconcile arc data with observations, as could not account for the observed increase in degree lengths toward the poles, ultimately necessitating more advanced ellipsoidal models in subsequent centuries.

19th Century Developments

In the early 19th century, the meridian arc measurement initiated by Jean-Baptiste Joseph Delambre and Pierre Méchain from 1792 to 1798, spanning approximately 9°21' of latitude from to , was refined to establish the foundational length for the , defining the meter as one ten-millionth of the distance from the to the along the . This effort, published in Base du système métrique décimal (1806–1810), provided precise geodetic data that confirmed the Earth's oblateness through and astronomical observations, though initial calculations underestimated the arc length due to measurement challenges in . A major advancement came with the , led by Friedrich Georg Wilhelm Struve from 1816 to 1855, which measured a meridian segment spanning 25°20' of latitude—approximately 2,820 km—from Hammerfest in to Staro-Nekrassowka near the , involving 265 triangulation points across ten countries. This extensive survey, the first accurate long-arc measurement, yielded an Earth's flattening estimate of 1:294.73 with a semi-major axis of 6,378,398 meters, significantly improving global understanding of the planet's ellipsoidal shape and supporting topographic mapping in the . In 1830, Friedrich Wilhelm Bessel developed an ellipsoidal model based on the Prussian triangulation survey of (1831–1832), directing meridian arc measurements that deduced an Earth's ellipticity of 1/299 in 1841; the resulting Bessel ellipsoid, with semi-major axis 6,377,397.155 meters and inverse flattening 299.15281, became a reference for northern European . Concurrently, proposed his 1830 ellipsoid tailored to the , featuring a semi-major axis of 6,377,563.396 meters and inverse flattening of 299.32496, optimizing fit for local surveys and later underpinning the Ordnance Survey's mapping systems. These 19th-century efforts, combining arcs like those of Delambre-Méchain and Struve with regional models from Bessel and Airy, collectively confirmed the Earth's oblateness and converged on a value of approximately 1/300, resolving earlier discrepancies and transitioning from spherical approximations to robust ellipsoidal frameworks.

Standardization of the Nautical Mile

The originated in the 16th and 17th centuries as the length corresponding to one minute of arc (1/60 of a ) along a , based on the assumption of a , yielding approximately 1852 meters. This definition stemmed from early efforts to divide the Earth's circumference into 21,600 equal parts, where each part represented one , facilitating by aligning distance with angular measurements of . Specifically, the equated to 1/21,600 of the full circumference, providing a practical unit for seafarers despite variations due to Earth's oblateness. In the , meridian arc measurements refined this unit, with the British Admiralty adopting a standardized value of 6,080 feet (approximately 1,853.184 meters) around the , drawing on geodesic data from the late 18th and early 19th centuries that informed the metric system's meridian-based definitions. These refinements accounted for the Earth's ellipsoidal shape, using surveys like those establishing the Clarke spheroid of 1866 to adjust the length of a mean minute of . The relation to the quarter meridian arc—equator to —positioned one as 1/5,400 of that under the spherical , though ellipsoidal models introduced slight variations for precision in nautical charts. International efforts culminated in the First International Extraordinary Hydrographic Conference in in 1929, where the was standardized at exactly 1,852 meters to harmonize global navigation and eliminate discrepancies from national arc measurements. This value represented a practical mean derived from contemporary meridian arc data, adopted by many nations for hydrographic purposes. By 1954, the international nautical mile was decoupled from ongoing geodesic refinements and fixed definitively at 1,852 meters, as affirmed by the United States and later by the United Kingdom in 1970, ensuring consistency in aviation and maritime applications independent of evolving Earth models. This shift prioritized uniformity over dynamic arc-based calculations, reflecting the maturation of 19th-century survey techniques into a stable global standard.

Mathematical Calculation

Arc Length Integral

The meridian arc length on an ellipsoidal model of Earth is computed using the differential arc length element along a line of constant . This element is given by ds = M(\varphi) \, d\varphi, where \varphi is the geodetic and M(\varphi) is the meridional , expressed as M(\varphi) = \frac{a (1 - e^2)}{(1 - e^2 \sin^2 \varphi)^{3/2}}, with a denoting the semi-major axis of the ellipsoid. This radius quantifies the local in the north-south direction at latitude \varphi, varying due to the ellipsoid's shape. The arc length s(\varphi) from the equator (\varphi = 0) to latitude \varphi is then the definite integral s(\varphi) = \int_0^\varphi M(\alpha) \, d\alpha = a (1 - e^2) \int_0^\varphi \frac{d\alpha}{(1 - e^2 \sin^2 \alpha)^{3/2}}. This form arises directly from integrating the differential element along the meridian. The squared eccentricity e^2 parametrizes the ellipsoid's deviation from sphericity, defined as e^2 = f(2 - f), where f = (a - b)/a is the flattening and b is the semi-minor axis. This parameter captures the oblateness caused by Earth's rotation, with smaller e^2 values (e.g., approximately 0.0067 for modern reference ellipsoids like WGS84) indicating near-sphericity, while increasing e^2 elongates the polar flattening.

Connection to Elliptic Integrals

The meridian arc length on an oblate spheroid can be expressed using the incomplete elliptic integral of the second kind after transformation to reduced latitude. The reduced (parametric) latitude \beta is related to the geodetic latitude \varphi by
\beta = \tan^{-1} \left( \sqrt{1 - e^2} \tan \varphi \right).
The arc length is then given by
s(\varphi) = a \left[ E(\beta, e) - e^2 \frac{\sin \varphi \cos \varphi}{\sqrt{1 - e^2 \sin^2 \varphi}} \right],
where E(\beta, e) = \int_0^\beta \sqrt{1 - e^2 \sin^2 \theta} \, d\theta is the incomplete elliptic integral of the second kind with modulus e. This form captures the geometric distortion due to Earth's oblateness through the parametric representation of the ellipsoid.
Key properties of E(\beta, e) include its smoothness over the integration domain for $0 \leq e < 1, ensuring no singularities along the path since the integrand remains positive and bounded. Unlike the derived elliptic functions, which exhibit periodicity with periods related to the complete integrals, the incomplete integral itself is monotonically increasing but non-periodic. For the quarter arc from the to the (\varphi = \pi/2, \beta = \pi/2), the correction term vanishes, and it reduces to the complete E(e) = E(\pi/2, e), yielding s = a E(e) \approx 10{,}001.966 for modern models like WGS84. The connection between meridian arcs and elliptic integrals was recognized in the , with applying these to problems in his 1811 work on integral calculus, linking ellipsoidal arc lengths to advanced analysis. further advanced the field around 1818 through transformations like the arithmetic-geometric mean, facilitating precise geodetic computations essential for determining Earth's figure.

Series Expansion Methods

Eccentricity-Based Expansions

Eccentricity-based expansions approximate the meridian arc length by treating the Earth's squared eccentricity e^2 as a small parameter, enabling a power series representation derived from the binomial expansion of the integrand in the arc length integral. The meridian arc s(\phi) from the equator to geodetic latitude \phi (in radians) on an oblate ellipsoid is given by s(\phi) = a (1 - e^2) \int_0^\phi (1 - e^2 \sin^2 \theta)^{-3/2} \, d\theta, where a is the semi-major axis and e is the first eccentricity. Expanding the integrand (1 - e^2 \sin^2 \theta)^{-3/2} using the generalized binomial theorem yields a series in powers of e^2 multiplied by even powers of \sin \theta, which integrate to trigonometric polynomials in \phi. This results in the general form s(\phi) = a \left[ A_0 \phi + \sum_{n=1}^\infty A_{2n} \sin(2n \phi) \right], where the coefficients A_n are functions of e^2, with alternating signs in the sum for typical truncations. The elliptic integral of the second kind E(\phi, e) = \int_0^\phi \sqrt{1 - e^2 \sin^2 \theta} \, d\theta, closely related to the meridian arc via differentiation and , admits a similar expansion: E(\phi, e) \approx \phi + \frac{e^2}{4} \left( \phi - \frac{\sin 2\phi}{2} \right) + \frac{3 e^4}{64} \left( \phi - \frac{6 \sin 2\phi}{2} + \frac{\sin 4\phi}{4} \right) + O(e^6). This form highlights the perturbative correction to the spherical case (e=0), with terms up to O(e^4) capturing the leading oblateness effects. The meridian arc itself derives from a related , but the shared binomial expansion structure ensures analogous series behavior. Jean-Baptiste Joseph Delambre developed the foundational eccentricity-based series in 1799 during the French meridian survey, deriving explicit coefficients up to order e^4 via direct expansion of the integrand and term-by-term . His series takes the form s(\phi) = a \left[ A_0 \phi + A_2 \sin 2\phi + A_4 \sin 4\phi \right], with A_0 = 1 - \frac{e^2}{4} - \frac{3 e^4}{64}, \quad A_2 = -\frac{3 e^2}{8} + \frac{3 e^4}{128}, \quad A_4 = \frac{15 e^4}{512}. Higher-order terms follow recursively, with coefficients involving coefficients adjusted for the -3/2 power. Delambre's formulation provided essential accuracy for 19th-century geodetic computations, influencing subsequent models. These expansions converge for e < 0.1, encompassing the Earth's value of approximately 0.0817 for the WGS84 . Truncation at order e^4 yields errors below 1 meter for quarter-meridian arcs, while inclusion of terms up to e^6 or e^8 reduces global arc errors to less than 1 mm, sufficient for high-precision and . For example, on the GRS80 (a = 6378137 m, e \approx 0.08169), the series to e^6 matches numerical to within 0.1 mm over the full polar distance.

Flattening-Based Expansions

Flattening-based expansions for the meridian arc length employ the third flattening n = \frac{a - b}{a + b}, where a is the semi-major axis and b the semi-minor axis of the , as the small parameter for series development. For small values of the first flattening f = \frac{a - b}{a}, this simplifies to n \approx \frac{f}{2}, providing a parameter that is roughly half the size of f, which enhances in computations for ellipsoids like Earth's. The meridian arc length s(\phi) from the to geodetic \phi can be expressed using the parametric \beta, defined such that \tan \beta = \sqrt{1 - e^2} \tan \phi where e is the first . The series takes the form s(\phi) = a (1 - n) \left[ B_0 \beta + B_2 \sin(2\beta) + B_4 \sin(4\beta) + \cdots \right], with coefficients beginning as B_0 = 1 + \frac{1}{4} n + \frac{1}{64} n^3 + \cdots and B_2 = -\left( \frac{3}{8} - \frac{3}{32} n + \cdots \right). This parameterization leverages the parametric for smoother trigonometric terms, facilitating convergence. In the , Friedrich Robert Helmert developed a foundational series up to order n^3, incorporating terms like those in B_2 for improved precision over earlier eccentricity-based approaches, as detailed in his work on higher . These expansions require fewer terms to achieve sub-millimeter accuracy for Earth's ellipsoid, where n \approx 0.00167 for the WGS84 parameters. The advantages of n-based series include faster for moderate values typical of planetary , reducing computational demands while maintaining high . They are employed in modern geodetic applications, including GPS coordinate transformations and ellipsoid distance calculations in libraries like GeographicLib.

Parametric Latitude Expansions

The parametric latitude β, also known as reduced latitude, is defined by the relation \tan \beta = (1 - f) \tan \phi, where \phi is the geodetic and f is the of the reference . This auxiliary latitude parameterizes the ellipse via x = a \cos \beta and z = b \sin \beta, where a and b are the , facilitating transformations between the ellipsoid and auxiliary surfaces. The meridian arc length s from the to geodetic \phi can be expressed directly in terms of the parametric \beta as s = a \int_0^\beta \sqrt{1 - e^2 \cos^2 u} \, du, where a is the semi-major axis, and e is the first related to the third n = f / (2 - f) by e^2 = 4n / (1 + n)^2. This form arises from the differential element on in parametric coordinates, ds = a \sqrt{1 - e^2 \cos^2 u} \, du. A of the integrand via the , followed by term-by-term integration, produces s \approx a \sqrt{1 - e^2} \left[ \beta + \frac{e^2}{4} \left( \frac{\sin 2\beta}{2} - \beta \right) + \frac{3 e^4}{64} \left( \frac{3 \sin 4\beta}{8} - \sin 2\beta - \frac{\sin 2\beta}{2} + \beta \right) + \cdots \right], adjusting for the form \sqrt{(1 - e^2) + e^2 \sin^2 u}. This Fourier-like series converges rapidly for typical ellipsoids, with higher-order terms involving \sin(6\beta)/6, etc., derived from powers of \sin^2 u. In the , advanced the application of parametric in conformal cartographic mappings, developing explicit series terms akin to these for projecting the onto the while preserving angles, as detailed in his work on the Hanoverian land survey . As n \to 0, the series reduces to the spherical s \approx a \beta \approx a \phi, confirming its consistency with elementary . This property, combined with the series' structure, makes parametric latitude expansions ideal for iterative algorithms in latitude-to-arc conversions and inversions, particularly in map projections and navigation systems.

Numerical and Generalized Series

Generalized series expansions for the meridian arc length s(\phi) extend the basic forms by incorporating higher-order terms in the e or the auxiliary flattening n = \frac{a - b}{a + b}, where a and b are the of the . These series provide improved accuracy for practical computations without relying on elliptic integrals. One common form expresses s(\phi) using even multiples as s(\phi) = a (1 - e^2) \sum_{k=0}^{m} B_k \left[ \phi \delta_{k0} + (-1)^k \frac{\sin(2k \phi)}{2k} \right], but standard extensions of Delambre follow s(\phi) = a (1 - e^2) \left[ \left(1 + \frac{3}{4} e^2 + \frac{45}{64} e^4 + \frac{175}{256} e^6 + \cdots \right) \phi - \left( \frac{3}{8} e^2 + \frac{15}{32} e^4 + \frac{105}{512} e^6 + \cdots \right) \sin 2\phi + \left( \frac{15}{512} e^4 + \frac{105}{2048} e^6 + \cdots \right) \sin 4\phi - \cdots \right], with coefficients up to order 6 or higher. Such expansions, often truncated at 10 terms, achieve sub-millimeter precision for Earth-based ellipsoids and are suitable for projections and . Numerical approximations further simplify these computations through closed-form expressions. Vincenty's 1975 method employs auxiliary angles, such as the reduced V where \tan V = (1 - f) \tan \phi with flattening f, to derive the via nested equations for the distance, reducing to the case when longitudes coincide. The formula is s = b A (u - \delta u), where b is the semi-minor axis, u is the auxiliary , A = 1 + \frac{u^2}{16384} [4096 + u^2 (-768 + u^2 (320 - 175 u^2))], and \delta u corrects for ellipticity using additional series terms. This approach yields accuracy better than 0.01 mm over distances up to 18,000 km. For even higher precision, Karney's 2013 algorithms introduce series expansions in n exceeding 20 terms, incorporating the authalic latitude \beta defined by \tan \beta = \sqrt{1 - e^2} \tan \phi to ensure uniform accuracy across latitudes. The meridian distance is computed as I_1(\sigma) = A_1 (\sigma + \sum_{l=1}^{16} C_{1l} \sin 2l \sigma), with coefficients like A_1 = (1 - \epsilon)^{-1} (1 + \frac{1}{4} \epsilon^2 + \frac{1}{64} \epsilon^4 + \frac{1}{256} \epsilon^6 + \cdots) and C_{11} = -\frac{1}{2} \epsilon + \frac{3}{16} \epsilon^3 - \frac{1}{32} \epsilon^5 + \cdots, where \epsilon relates to n. Accurate to order f^6 (with f \approx 1/298), these yield global errors under 0.1 mm. Implementations in libraries such as GeographicLib optimize these series to avoid evaluations, enabling rapid computation in software for and GIS applications.

Meridian Perimeters

Quarter Meridian Arc

The quarter meridian arc represents the length of the meridian curve from the to the (or equivalently to the ) on an oblate of revolution modeling the . This arc length, denoted s(90^\circ), is fundamentally expressed as s(90^\circ) = a E(e), where a is the semi-major axis of the , e is its first , and E(e) = \int_0^{\pi/2} \sqrt{1 - e^2 \sin^2 \theta} \, d\theta is the complete of the second kind. For the WGS84 ellipsoid, with a = 6{,}378{,}137 m and e^2 \approx 0.00669438, the quarter meridian arc measures approximately 10,001.9657 km. This value exceeds the simplified spherical approximation of 10,000 km by about 1.97 km, reflecting the ellipsoid's flattening, which elongates the polar meridian relative to a naive equatorial-radius sphere but aligns closely with the precise \pi a / 2 \approx 10{,}001.966 km for an undistorted sphere of radius a. Historically, the quarter meridian arc held pivotal importance in establishing length standards. Early proposals, formalized by the in 1791, defined the meter as exactly one ten-millionth of this along the , aiming to tie measurement to Earth's geometry for universality. The 1866 U.S. Metric Act further linked customary units to this standard by defining the yard as 3600/3937 meters (approximately 0.914402 m), thereby indirectly basing the yard on quarter meridian measurements through the meter's origin. Series expansions provide a practical means to compute the quarter meridian arc without evaluating the elliptic integral directly. Substituting \phi = 90^\circ (or \pi/2 radians) into the general meridian arc series simplifies the expression, as higher-order sine terms vanish, yielding s(90^\circ) = a \left(1 - \frac{e^2}{4} - \frac{3 e^4}{64} - \frac{5 e^6}{256} - \cdots \right) \frac{\pi}{2}. This eccentricity-based expansion converges rapidly for Earth's small e^2, with the first few terms sufficing for sub-millimeter accuracy on WGS84.

Full Polar Perimeter

The full polar perimeter represents the complete closed path along a ellipse on an oblate spheroid, encircling the poles due to the of the ellipsoid. This perimeter P is four times the length of the quarter meridian arc from to , given by the P = 4 a E(e), where a is the semi-major axis and E(e) = \int_0^{\pi/2} \sqrt{1 - e^2 \sin^2 \theta} \, d\theta is the complete of the second kind, with e denoting the . For the WGS84 reference ellipsoid, the full polar perimeter measures approximately 40,007.862 km, in contrast to the equatorial circumference of roughly 40,075 km, highlighting the ellipsoid's oblateness that shortens polar-relative distances. This value underscores the 's role as a fundamental measure in geodetic modeling, where the quarter meridian length, as detailed in prior sections, scales directly to the full perimeter. Geometrically, the meridian forms an ellipse in the plane containing the , with perimeter determined by the varying —maximal at the and minimal at the poles—preventing it from being a perfect circle despite the closed path. This structure arises from the ellipsoid's definition, where the meridian shares the same e as the generating .

Inverse Meridian Problem

Problem Statement

The problem in involves determining the geodetic \phi corresponding to a given s measured along a from a point on the surface of a ellipsoid, typically starting from the equator where \phi = 0. This task is essential for transforming linear distances into angular coordinates in ellipsoidal models of the Earth. The mathematical formulation requires solving for \phi in the equation s = a (1 - e^2) \int_0^\phi \frac{d\alpha}{(1 - e^2 \sin^2 \alpha)^{3/2}}, where a is the semi-major axis of the and e^2 is its squared first eccentricity; this integral arises from the along the . The is transcendental and cannot be inverted in closed form using elementary functions, as it involves an incomplete of the second kind, demanding numerical iteration or series reversion for solution. Variants of the problem extend to arc lengths between arbitrary latitudes \phi_1 and \phi_2, where s = s(\phi_2) - s(\phi_1), or to paths along any constant- meridian, such as the at longitude 0°, due to the axisymmetric nature of the . This problem holds critical importance in geodetic applications, including precise positioning in , development of map projections like the Universal Transverse Mercator (UTM) system, and coordinate transformations in global navigation satellite systems.

Solution Approaches

The inverse meridian problem, which determines the geodetic latitude \phi from a given arc length s along an ellipsoid's meridian, can be addressed through several established numerical and analytical techniques. Iterative methods, such as the Newton-Raphson algorithm, are commonly employed by applying it to the forward meridian arc integral. Starting with an initial guess \phi_0 \approx s/a, where a is the semi-major axis, the iteration refines the estimate using the update \phi_{n+1} = \phi_n - (M(\phi_n) - s)/M'(\phi_n), where M(\phi) is the meridian arc from the equator to \phi and M'(\phi) = a (1 - e^2) / (1 - e^2 \sin^2 \phi)^{3/2} is its derivative with respect to \phi, with e the eccentricity. This approach typically converges in two iterations to high precision, such as 0.0001 radians, for ellipsoids like Krasovsky's. Series inversion methods provide closed-form approximations by expanding \phi in powers of the reduced arc length u = s / [a (1 - e^2)], often using the third flattening n = (a - b)/(a + b) for improved convergence over eccentricity-based series. A representative expansion is \phi = u + \sum_{j=1}^{m} a_j \sin(2j u), where coefficients a_j are polynomials in e^2 up to order 10, such as a_2 = (3/8)e^2 + (3/16)e^4 + (213/2048)e^6 + \cdots. These series, derived via or , achieve accuracies better than $10^{-7} arcseconds when truncated appropriately and are particularly useful in map projections like Gauss-Krüger. For an exact solution, the inverse can leverage elliptic function theory, as the meridian arc corresponds to the incomplete elliptic integral of the second kind via the parametric latitude \beta, where \tan \beta = \sqrt{1 - e^2} \tan \phi and s = a E(\beta, e), with E(\beta, k) = \int_0^\beta \sqrt{1 - k^2 \sin^2 \theta} \, d\theta. Inversion requires first solving for \beta numerically or via series (since direct inversion of E is non-elementary), then obtaining \phi = \arctan\left( \frac{\tan \beta}{\sqrt{1 - e^2}} \right). This formulation, while theoretically precise, requires numerical evaluation and is less common in practice compared to series or iteration. Modern algorithms enhance efficiency and robustness, exemplified by Karney's 2013 method, which solves the general inverse problem (including meridians as the zero longitude-difference case) via Newton's on the reduced length parameter, augmented by expansions to order f^6 (flattening) and rational approximations for auxiliary integrals. This yields accuracies exceeding $10^{-11} radians in for Earth-like ellipsoids, converging in 2–4 even for near-antipodal points, outperforming earlier methods like Vincenty's. Implementations of these approaches are available in geospatial software for real-time . The GeographicLib provides C++ and routines based on Karney's algorithms, supporting high-precision inverse meridian calculations with full double-precision fidelity. Similarly, the PROJ incorporates inverse meridian arc functions using series or iterative solvers, integrated into its cartographic toolkit for coordinate transformations.

References

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    ### Document Details
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    ### Summary of Meridian Distance Formulas and Historical Context
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