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#include "erfa.h" |
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int eraGc2gde ( double a, double f, double xyz[3], |
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double *elong, double *phi, double *height ) |
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/* |
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** - - - - - - - - - - |
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** e r a G c 2 g d e |
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** - - - - - - - - - - |
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** |
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** Transform geocentric coordinates to geodetic for a reference |
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** ellipsoid of specified form. |
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** |
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** Given: |
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** a double equatorial radius (Notes 2,4) |
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** f double flattening (Note 3) |
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** xyz double[3] geocentric vector (Note 4) |
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** |
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** Returned: |
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** elong double longitude (radians, east +ve) |
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** phi double latitude (geodetic, radians) |
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** height double height above ellipsoid (geodetic, Note 4) |
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** |
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** Returned (function value): |
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** int status: 0 = OK |
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** -1 = illegal f |
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** -2 = illegal a |
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** |
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** Notes: |
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** |
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** 1) This function is based on the GCONV2H Fortran subroutine by |
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** Toshio Fukushima (see reference). |
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** |
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** 2) The equatorial radius, a, can be in any units, but meters is |
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** the conventional choice. |
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** |
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** 3) The flattening, f, is (for the Earth) a value around 0.00335, |
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** i.e. around 1/298. |
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** |
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** 4) The equatorial radius, a, and the geocentric vector, xyz, |
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** must be given in the same units, and determine the units of |
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** the returned height, height. |
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** |
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** 5) If an error occurs (status < 0), elong, phi and height are |
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** unchanged. |
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** |
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** 6) The inverse transformation is performed in the function |
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** eraGd2gce. |
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** |
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** 7) The transformation for a standard ellipsoid (such as ERFA_WGS84) can |
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** more conveniently be performed by calling eraGc2gd, which uses a |
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** numerical code to identify the required A and F values. |
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** |
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** Reference: |
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** |
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** Fukushima, T., "Transformation from Cartesian to geodetic |
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** coordinates accelerated by Halley's method", J.Geodesy (2006) |
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** 79: 689-693 |
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** |
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** Copyright (C) 2013-2019, NumFOCUS Foundation. |
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** Derived, with permission, from the SOFA library. See notes at end of file. |
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*/ |
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{ |
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double aeps2, e2, e4t, ec2, ec, b, x, y, z, p2, absz, p, s0, pn, zc, |
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c0, c02, c03, s02, s03, a02, a0, a03, d0, f0, b0, s1, |
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cc, s12, cc2; |
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/* ------------- */ |
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/* Preliminaries */ |
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/* ------------- */ |
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/* Validate ellipsoid parameters. */ |
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if ( f < 0.0 || f >= 1.0 ) return -1; |
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if ( a <= 0.0 ) return -2; |
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/* Functions of ellipsoid parameters (with further validation of f). */ |
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aeps2 = a*a * 1e-32; |
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e2 = (2.0 - f) * f; |
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e4t = e2*e2 * 1.5; |
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ec2 = 1.0 - e2; |
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if ( ec2 <= 0.0 ) return -1; |
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ec = sqrt(ec2); |
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b = a * ec; |
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/* Cartesian components. */ |
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x = xyz[0]; |
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y = xyz[1]; |
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z = xyz[2]; |
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/* Distance from polar axis squared. */ |
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p2 = x*x + y*y; |
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/* Longitude. */ |
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*elong = p2 > 0.0 ? atan2(y, x) : 0.0; |
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/* Unsigned z-coordinate. */ |
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absz = fabs(z); |
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/* Proceed unless polar case. */ |
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if ( p2 > aeps2 ) { |
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/* Distance from polar axis. */ |
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p = sqrt(p2); |
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/* Normalization. */ |
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s0 = absz / a; |
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pn = p / a; |
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zc = ec * s0; |
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/* Prepare Newton correction factors. */ |
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c0 = ec * pn; |
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c02 = c0 * c0; |
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c03 = c02 * c0; |
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s02 = s0 * s0; |
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s03 = s02 * s0; |
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a02 = c02 + s02; |
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a0 = sqrt(a02); |
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a03 = a02 * a0; |
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d0 = zc*a03 + e2*s03; |
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f0 = pn*a03 - e2*c03; |
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/* Prepare Halley correction factor. */ |
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b0 = e4t * s02 * c02 * pn * (a0 - ec); |
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s1 = d0*f0 - b0*s0; |
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cc = ec * (f0*f0 - b0*c0); |
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/* Evaluate latitude and height. */ |
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*phi = atan(s1/cc); |
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s12 = s1 * s1; |
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cc2 = cc * cc; |
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*height = (p*cc + absz*s1 - a * sqrt(ec2*s12 + cc2)) / |
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sqrt(s12 + cc2); |
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} else { |
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/* Exception: pole. */ |
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*phi = ERFA_DPI / 2.0; |
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*height = absz - b; |
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} |
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140
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/* Restore sign of latitude. */ |
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if ( z < 0 ) *phi = -*phi; |
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/* OK status. */ |
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return 0; |
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} |
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/*---------------------------------------------------------------------- |
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** |
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** |
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** Copyright (C) 2013-2019, NumFOCUS Foundation. |
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** All rights reserved. |
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** |
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** This library is derived, with permission, from the International |
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** Astronomical Union's "Standards of Fundamental Astronomy" library, |
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** available from http://www.iausofa.org. |
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** |
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** The ERFA version is intended to retain identical functionality to |
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** the SOFA library, but made distinct through different function and |
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** file names, as set out in the SOFA license conditions. The SOFA |
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** original has a role as a reference standard for the IAU and IERS, |
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** and consequently redistribution is permitted only in its unaltered |
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** state. The ERFA version is not subject to this restriction and |
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** therefore can be included in distributions which do not support the |
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** concept of "read only" software. |
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** |
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** Although the intent is to replicate the SOFA API (other than |
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** replacement of prefix names) and results (with the exception of |
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** bugs; any that are discovered will be fixed), SOFA is not |
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** responsible for any errors found in this version of the library. |
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** |
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** If you wish to acknowledge the SOFA heritage, please acknowledge |
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** that you are using a library derived from SOFA, rather than SOFA |
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** itself. |
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** |
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** |
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** TERMS AND CONDITIONS |
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** |
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** Redistribution and use in source and binary forms, with or without |
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** modification, are permitted provided that the following conditions |
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** are met: |
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** |
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** 1 Redistributions of source code must retain the above copyright |
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** notice, this list of conditions and the following disclaimer. |
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** |
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** 2 Redistributions in binary form must reproduce the above copyright |
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** notice, this list of conditions and the following disclaimer in |
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** the documentation and/or other materials provided with the |
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** distribution. |
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** |
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** 3 Neither the name of the Standards Of Fundamental Astronomy Board, |
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** the International Astronomical Union nor the names of its |
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** contributors may be used to endorse or promote products derived |
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** from this software without specific prior written permission. |
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** |
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** THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS |
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** "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT |
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** LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS |
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** FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE |
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** COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, |
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** INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, |
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** BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; |
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** LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER |
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** CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT |
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** LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN |
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** ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
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** POSSIBILITY OF SUCH DAMAGE. |
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** |
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*/ |