# Coverage for pygeodesy/ecef.py : 94%

## 309 statements 289 run 20 missing 9 excluded

Hot-keys on this page

r m x p toggle line displays

j k next/prev highlighted chunk

0 (zero) top of page

1 (one) first highlighted chunk

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 374 375 376 377 378 379 380 381 382 383 384 385 386 387 388 389 390 391 392 393 394 395 396 397 398 399 400 401 402 403 404 405 406 407 408 409 410 411 412 413 414 415 416 417 418 419 420 421 422 423 424 425 426 427 428 429 430 431 432 433 434 435 436 437 438 439 440 441 442 443 444 445 446 447 448 449 450 451 452 453 454 455 456 457 458 459 460 461 462 463 464 465 466 467 468 469 470 471 472 473 474 475 476 477 478 479 480 481 482 483 484 485 486 487 488 489 490 491 492 493 494 495 496 497 498 499 500 501 502 503 504 505 506 507 508 509 510 511 512 513 514 515 516 517 518 519 520 521 522 523 524 525 526 527 528 529 530 531 532 533 534 535 536 537 538 539 540 541 542 543 544 545 546 547 548 549 550 551 552 553 554 555 556 557 558 559 560 561 562 563 564 565 566 567 568 569 570 571 572 573 574 575 576 577 578 579 580 581 582 583 584 585 586 587 588 589 590 591 592 593 594 595 596 597 598 599 600 601 602 603 604 605 606 607 608 609 610 611 612 613 614 615 616 617 618 619 620 621 622 623 624 625 626 627 628 629 630 631 632 633 634 635 636 637 638 639 640 641 642 643 644 645 646 647 648 649 650 651 652 653 654 655 656 657 658 659 660 661 662 663 664 665 666 667 668 669 670 671 672 673 674 675 676 677 678 679 680 681 682 683 684 685 686 687 688 689 690 691 692 693 694 695 696 697 698 699 700 701 702 703 704 705 706 707 708 709 710 711 712 713 714 715 716 717 718 719 720 721 722 723 724 725 726 727 728 729 730 731 732 733 734 735 736 737 738 739 740 741 742 743 744 745 746 747 748 749 750 751 752 753 754 755 756 757 758 759 760 761 762 763 764 765 766 767 768 769 770 771 772 773 774 775 776 777 778 779 780 781 782 783 784 785 786 787 788 789 790 791 792 793 794 795 796 797 798 799 800 801 802 803 804 805 806 807 808 809 810 811 812 813 814 815 816 817 818 819 820 821 822 823 824 825 826 827 828 829 830 831 832 833 834 835 836 837 838 839 840 841 842 843 844 845 846 847 848 849 850 851 852 853 854 855 856 857 858 859 860 861 862 863 864 865 866 867 868 869 870 871 872 873 874 875 876 877 878 879 880 881 882 883 884 885 886 887 888 889 890 891 892 893 894 895 896 897 898 899 900 901 902 903 904 905 906 907 908 909 910 911 912 913 914 915 916 917 918 919 920 921 922 923 924 925 926 927 928 929 930 931 932 933 934 935 936 937 938 939 940 941 942 943 944 945 946 947 948 949 950 951 952 953 954 955 956 957 958 959 960 961 962 963 964 965 966 967 968 969 970 971 972 973 974 975 976 977 978 979 980 981 982 983 984 985 986 987 988 989 990 991 992 993 994 995 996 997 998 999 1000 1001 1002 1003 1004 1005 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1017 1018 1019 1020 1021 1022 1023 1024 1025 1026 1027 1028 1029 1030 1031 1032 1033 1034 1035 1036 1037 1038 1039 1040 1041 1042 1043 1044 1045 1046 1047 1048 1049 1050 1051 1052 1053 1054 1055 1056 1057 1058 1059 1060 1061 1062 1063 1064 1065 1066 1067 1068 1069 1070 1071 1072 1073 1074 1075 1076 1077 1078 | # -*- coding: utf-8 -*- u'''Geocentric conversions transcribed from I{Charles Karney}'s C++ classes U{Geocentric <https://GeographicLib.SourceForge.io/html/classGeographicLib_1_1Geocentric.html>} and U{LocalCartesian<https://GeographicLib.SourceForge.io/html/classGeographicLib_1_1LocalCartesian.html>} into pure Python classes L{EcefKarney} respectively L{EcefCartesian}, class L{EcefVeness} transcribed from I{Chris Veness}' JavaScript classes U{LatLonEllipsoidal, Cartesian <https://www.Movable-Type.co.UK/scripts/geodesy/docs/latlon-ellipsoidal.js.html>} and class L{EcefYou} implementing I{Rey-Jer You}'s U{transformations <https://www.ResearchGate.net/publication/240359424>}. Convert between geodetic coordinates C{lat}-, C{lon}gitude and height C{h} (measured vertically from the surface of the ellipsoid) to geocentric C{x}, C{y} and C{z} coordinates, also known as I{Earth-Centered, Earth-Fixed} (U{ECEF<https://WikiPedia.org/wiki/ECEF>}). The origin of geocentric coordinates is at the center of the earth. The C{z} axis goes thru the North pole, C{lat} = 90°. The C{x} axis goes thru C{lat} = 0°, C{lon} = 0°. The origin of local cartesian coordinate system is at C{lat0}, C{lon0} and C{height0}. The C{z} axis is normal to the ellipsoid, the C{y} axis points due North. The plane C{z = -height0} is tangent to the ellipsoid. Forward conversion from geodetic to geocentric (ECEF) coordinates is straightforward. For the reverse transformation we use Hugues Vermeille's U{Direct transformation from geocentric coordinates to geodetic coordinates <https://DOI.org/10.1007/s00190-002-0273-6>}, J. Geodesy (2002) 76, 451-454. Several changes have been made to ensure that the method returns accurate results for all finite inputs (even if h is infinite). The changes are described in Appendix B of C. F. F. Karney U{Geodesics on an ellipsoid of revolution<https://ArXiv.org/abs/1102.1215v1>}, Feb. 2011, 85, 105-117 (U{preprint<https://ArXiv.org/abs/1102.1215v1>}). Vermeille similarly updated his method in U{An analytical method to transform geocentric into geodetic coordinates<https://DOI.org/10.1007/s00190-010-0419-x>}, J. Geodesy (2011) 85, 105-117. See U{Geocentric coordinates <https://GeographicLib.SourceForge.io/html/geocentric.html>} for more information. The errors in these routines are close to round-off. Specifically, for points within 5,000 km of the surface of the ellipsoid (either inside or outside the ellipsoid), the error is bounded by 7 nm (7 nanometers) for the WGS84 ellipsoid. See U{Geocentric coordinates<https://GeographicLib.SourceForge.io/html/geocentric.html>} for further information on the errors. ''' from pygeodesy.basics import EPS, EPS1, EPS_2, _IsNotError, isscalar, map1, \ property_RO, _TypeError from pygeodesy.datum import Datum, Datums, Ellipsoid from pygeodesy.fmath import cbrt, fdot, fsum_, hypot1 from pygeodesy.lazily import _ALL_DOCS, _ALL_LAZY from pygeodesy.named import LatLon2Tuple, LatLon3Tuple, LatLon4Tuple, \ _NamedBase, _NamedTuple, PhiLam2Tuple, Vector3Tuple, \ _xnamed from pygeodesy.streprs import unstr from pygeodesy.utily import degrees90, degrees180, sincos2, sincos2d from pygeodesy.vector3d import _xyzn4 from math import atan2, copysign, cos, degrees, hypot, radians, sqrt # all public contants, classes and functions __all__ = _ALL_LAZY.ecef + _ALL_DOCS('_EcefBase', 'Ecef9Tuple') __version__ = '20.03.12' class EcefError(ValueError): '''An ECEF or related issue. ''' pass def _llhn4(latlonh, lon, height, suffix): '''(INTERNAL) Get C{lat, lon, h, name} as C{4-tuple}. ''' try: llh = latlonh.lat, latlonh.lon, getattr(latlonh, 'height', getattr(latlonh, 'h', height)) except AttributeError: llh = latlonh, lon, height try: lat, lon, h = map1(float, *llh) except (TypeError, ValueError) as x: t = 'lat_, lon_ or height_'.replace('_', suffix) raise EcefError('%s invalid: %r, %s' % (t, llh, x)) if abs(lat) > 90: raise EcefError('%s%s out of range: %.6g' % ('lat', suffix, lat)) return lat, lon, h, getattr(latlonh, 'name', '') def _sch3(y, x): '''(INTERNAL) Compute sin, cos and hypotenuse. ''' h = hypot(y, x) if h > 0: # EPS_2 s, c = y / h, x / h else: s, c = 0, 1 return s, c, h class _EcefBase(_NamedBase): '''(INTERNAL) Base class for L{EcefKarney}, L{EcefVeness} and L{EcefYou}. ''' _datum = None _E = None def __init__(self, a_ellipsoid, f, name): '''(INTERNAL) New C{Ecef...}. ''' try: E = a_ellipsoid if f is None: if isinstance(E, Datum): self._datum = E E = E.ellipsoid elif not isinstance(E, Ellipsoid): raise TypeError self.name = E.name elif isscalar(E) and isscalar(f): a = float(E) f_ = (1.0 / f) if f else 0 # sphere b = None if f_ else a E = Ellipsoid(a, b, f_, name='_' + name) else: raise ValueError if not (E.a > 0 and E.f < 1): raise ValueError except (TypeError, ValueError): t = unstr(self.classname, a=E, f=f) raise EcefError('%s invalid: %s' % ('ellipsoid', t)) self._E = E if name: self.name = name @property_RO def a(self): '''Get C{E.a}, the major, equatorial radius (C{meter}). ''' return self._E.a equatorialRadius = a # Karney property @property_RO def datum(self): '''Get the datum (L{Datum}) or C{None}. ''' return self._datum @property_RO def ellipsoid(self): '''Get C{E}, the ellipsoid (L{Ellipsoid}). ''' return self._E @property_RO def f(self): '''Get C{E.f}, the flattening (C{float}), zero for sphere. ''' return self._E.f flattening = f # Karney property def _Matrix(self, sa, ca, sb, cb): '''Creation a rotation matrix. @return: A L{EcefMatrix}. ''' # This matrix is given by the following quaternion operations # qrot(lam, [0,0,1]) * qrot(phi, [0,-1,0]) * [1,1,1,1]/2 # or # qrot(pi/2 + lam, [0,0,1]) * qrot(-pi/2 + phi, [-1,0,0]) # where # qrot(t,v) = [cos(t/2), sin(t/2)*v[1], sin(t/2)*v[2], sin(t/2)*v[3]] # Local X axis (east) in geocentric coords # M[0] = -slam; M[3] = clam; M[6] = 0; # Local Y axis (north) in geocentric coords # M[1] = -clam * sphi; M[4] = -slam * sphi; M[7] = cphi; # Local Z axis (up) in geocentric coords # M[2] = clam * cphi; M[5] = slam * cphi; M[8] = sphi; return self._xnamed(EcefMatrix(sa, ca, sb, cb)) def toStr(self, prec=9): # PYCHOK signature '''Return this C{Ecef*} as a string. @keyword prec: Optional precision, number of decimal digits (0..9). @return: This C{Ecef*} representation (C{str}). ''' return self.attrs('a', 'f', 'datum', 'ellipsoid', 'name', prec=prec) # @property_RO # def xyz(self): # '''Get the geocentric C{(x, y, z)} coordinates (L{Vector3Tuple}C{(x, y, z)}). # ''' # return self._xnamed(Vector3Tuple(self.x, self.y, self.z)) class EcefKarney(_EcefBase): '''Conversion between geodetic and geocentric, aka I{Earth-Centered, Earth-Fixed} (ECEF) coordinates based on I{Karney}'s U{Geocentric <https://GeographicLib.SourceForge.io/html/classGeographicLib_1_1Geocentric.html>} methods. ''' _hmax = 0 def __init__(self, a_ellipsoid, f=None, name=''): '''New L{EcefKarney} converter. @param a_ellipsoid: An ellipsoid (L{Ellipsoid}), a datum (L{Datum}) or C{scalar} for the major, equatorial radius of the ellipsoid (C{meter}). @keyword f: C{None} or the ellipsoid flattening (C{scalar}), required for C{scalar} B{C{a_datum_ellipsoid}}, B{C{f}}=0 represents a sphere, negative B{C{f}} a prolate ellipsoid. @keyword name: Optional name (C{str}). @raise EcefError: If B{C{a_ellipsoid}} not L{Ellipsoid}, L{Datum} or C{scalar} or B{C{f}} not C{scalar} or if C{scalar} B{C{a_ellipsoid}} not positive or B{C{f}} not less than 1.0. ''' _EcefBase.__init__(self, a_ellipsoid, f, name) self._hmax = self.a / EPS_2 @property_RO def e2(self): '''Get C{E.f * (2 - E.f)}, 1st eccentricty squared (C{float}). ''' return self._E.e2 @property_RO def e2a(self): '''Get C{abs(E.e2)} (C{float}). ''' return abs(self._E.e2) @property_RO def e2m(self): '''Get C{1 - E.e2a} == C{(1 - E.f)**2} (C{float}). ''' return self._E.e12 # == (1 - E.f)**2 @property_RO def e4a(self): '''Get C{E.e2a**2} (C{float}). ''' return self._E.e4 def forward(self, latlonh, lon=None, height=0, M=False): '''Convert from geodetic C{(lat, lon, height)} to geocentric C{(x, y, z)}. @param latlonh: Either a C{LatLon}, an L{Ecef9Tuple} or C{scalar} latitude in C{degrees}. @keyword lon: Optional C{scalar} longitude in C{degrees} for C{scalar} B{C{latlonh}}. @keyword height: Optional height in C{meter}, vertically above (or below) the surface of the ellipsoid. @keyword M: Optionally, return the rotation L{EcefMatrix} (C{bool}). @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geocentric C{(x, y, z)} coordinates for the given geodetic ones C{(lat, lon, height)}, case C{C} 0, optional L{EcefMatrix} C{M} and C{datum} if available. @raise EcefError: If B{C{latlonh}} not C{LatLon}, L{Ecef9Tuple} or C{scalar} or B{C{lon}} not C{scalar} for C{scalar} B{C{latlonh}} or C{abs(B{lat})} exceeds 90°. @note: Let C{v} be a unit vector located at C{(lat, lon, h)}. We can express C{v} as column vectors in one of two ways, C{v1} in east, north, up coordinates (where the components are relative to a local coordinate system at C{C(lat0, lon0, h0)}) or as C{v0} in geocentric C{x, y, z} coordinates. Then, M{v0 = M ⋅ v1} where C{M} is the rotation matrix. ''' lat, lon, h, name = _llhn4(latlonh, lon, height, '') sa, ca, sb, cb = sincos2d(lat, lon) n = self.a / sqrt(1 - self.e2 * sa**2) z = (self.e2m * n + h) * sa x = (n + h) * ca m = self._Matrix(sa, ca, sb, cb) if M else None r = Ecef9Tuple(x * cb, x * sb, z, lat, lon, h, 0, m, self.datum) return self._xnamed(r, name) def reverse(self, xyz, y=None, z=None, M=False): '''Convert from geocentric C{(x, y, z)} to geodetic C{(lat, lon, height)}. @param xyz: Either an L{Ecef9Tuple}, an C{(x, y, z)} 3-tuple or C{scalar} ECEF C{x} coordinate in C{meter}. @keyword y: ECEF C{y} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{z}}. @keyword z: ECEF C{z} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{y}}. @keyword M: Optionally, return the rotation L{EcefMatrix} (C{bool}). @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geodetic coordinates C{(lat, lon, height)} for the given geocentric ones C{(x, y, z)}, case C{C}, optional L{EcefMatrix} C{M} and C{datum} if available. @raise EcefError: If B{C{xyz}} not L{Ecef9Tuple} or C{scalar} C{x} or B{C{y}} and/or B{C{z}} not C{scalar} for C{scalar} B{C{xyz}}. @note: In general, there are multiple solutions and the result which minimizes C{height} is returned, i.e., C{(lat, lon)} corresponds to the closest point on the ellipsoid. If there are still multiple solutions with different latitudes (applies only if C{z} = 0), then the solution with C{lat} > 0 is returned. If there are still multiple solutions with different longitudes (applies only if C{x} = C{y} = 0) then C{lon} = 0 is returned. The returned C{height} value is not below M{−E.a * (1 − E.e2) / sqrt(1 − E.e2 * sin(lat)**2)}. The returned C{lon} is in the range [−180°, 180°]. Like C{forward} above, M{v1 = Transpose(M) ⋅ v0}. ''' x, y, z, name = _xyzn4(xyz, y, z, Error=EcefError) sb, cb, d = _sch3(y, x) h = hypot(d, z) # distance to earth center if h > self._hmax: # We really far away (> 12 million light years). Treat the earth # as a point and h, above, is an acceptable approximation to the # height. This avoids overflow, e.g., in the computation of d # below. It's possible that h has overflowed to INF, that's OK. # Treat finite x, y, but r overflows to +INF by scaling by 2. sb, cb, r = _sch3(y / 2, x / 2) sa, ca, _ = _sch3(z / 2, r) C = 1 elif self.e4a: # Treat prolate spheroids by swapping R and Z here and by switching # the arguments to phi = atan2(...) at the end. p = (d / self.a)**2 q = self.e2m * (z / self.a)**2 if self.f < 0: p, q = q, p r = p + q - self.e4a e = self.e4a * q if e or r > 0: # Avoid possible division by zero when r = 0 by multiplying # equations for s and t by r^3 and r, resp. s = e * p / 4 # s = r^3 * s u = r = r / 6 r2 = r**2 r3 = r * r2 t3 = s + r3 disc = s * (r3 + t3) if disc < 0: # t is complex, but the way u is defined the result is real. # There are three possible cube roots. We choose the root # which avoids cancellation. Note, disc < 0 implies r < 0. u += 2 * r * cos(atan2(sqrt(-disc), -t3) / 3) else: # Pick the sign on the sqrt to maximize abs(T3). This # minimizes loss of precision due to cancellation. The # result is unchanged because of the way the T is used # in definition of u. if disc > 0: t3 += copysign(sqrt(disc), t3) # t3 = (r * t)^3 # N.B. cbrt always returns the real root, cbrt(-8) = -2. t = cbrt(t3) # t = r * t # t can be zero; but then r2 / t -> 0. if t: u += t + r2 / t v = sqrt(u**2 + e) # guaranteed positive # Avoid loss of accuracy when u < 0. Underflow doesn't occur in # E.e4 * q / (v - u) because u ~ e^4 when q is small and u < 0. uv = (e / (v - u)) if u < 0 else (u + v) # u+v, guaranteed positive # Need to guard against w going negative due to roundoff in uv - q. w = max(0.0, self.e2a * (uv - q) / (2 * v)) # Rearrange expression for k to avoid loss of accuracy due to # subtraction. Division by 0 not possible because uv > 0, w >= 0. k1 = k2 = uv / (sqrt(uv + w**2) + w) if self.f < 0: k1 -= self.e2 else: k2 += self.e2 sa, ca, h = _sch3(z / k1, d / k2) h *= k1 - self.e2m C = 2 else: # e = self.e4a * q == 0 and r <= 0 # This leads to k = 0 (oblate, equatorial plane) and k + E.e^2 = 0 # (prolate, rotation axis) and the generation of 0/0 in the general # formulas for phi and h, using the general formula and division # by 0 in formula for h. Handle this case by taking the limits: # f > 0: z -> 0, k -> E.e2 * sqrt(q) / sqrt(E.e4 - p) # f < 0: r -> 0, k + E.e2 -> -E.e2 * sqrt(q) / sqrt(E.e4 - p) q = self.e4a - p if self.f < 0: p, q, e = q, p, -1 else: e = -self.e2m sa, ca, h = _sch3(sqrt(q / self.e2m), sqrt(p)) h *= self.a * e / self.e2a if z < 0: sa = -sa # for tiny negative z, not for prolate C = 3 else: # self.e4a == 0 # Treat the spherical case. Dealing with underflow in the general # case with E.e2 = 0 is difficult. Origin maps to North pole, same # as with ellipsoid. sa, ca, _ = _sch3(z if h else 1, d) h -= self.a C = 4 r = Ecef9Tuple(x, y, z, degrees(atan2(sa, ca)), degrees(atan2(sb, cb)), h, C, self._Matrix(sa, ca, sb, cb) if M else None, self.datum) return self._xnamed(r, name) class EcefCartesian(_NamedBase): '''Conversion between geodetic C{(lat, lon, height)} and local cartesian C{(x, y, z)} coordinates with a local cartesian origin at C{(lat0, lon0, height0)} transcibed from on I{Karney}'s C++ class U{LocalCartesian <https://GeographicLib.SourceForge.io/html/classGeographicLib_1_1LocalCartesian.html>}. The C{z} axis is normal to the ellipsoid, the C{y} axis points due North. The plane C{z = -heighth0} is tangent to the ellipsoid. The conversions all take place via geocentric coordinates using a geocentric L{EcefKarney}, by default the WGS84 datum/ellipsoid. ''' _ecef = None _t0 = None def __init__(self, latlonh0=0, lon0=0, height0=0, ecef=EcefKarney(Datums.WGS84), name=''): '''New L{EcefCartesian} converter. @keyword latlonh0: Either a C{LatLon}, an L{Ecef9Tuple} or C{scalar} latitude in C{degrees} of the cartesian origin. @keyword lon0: Optional C{scalar} longitude of the cartesian origin in C{degrees} for C{scalar} B{C{latlonh0}}. @keyword height0: Optional height of the cartesian origin in C{meter}, vertically above (or below) the surface of the ellipsoid. @keyword ecef: An EXEC converter (L{EcefKarney}). @keyword name: Optional name (C{str}). @raise EcefError: If B{C{latlonh0}} not C{LatLon}, L{Ecef9Tuple} or C{scalar} or B{C{lon0}} not C{scalar} for C{scalar} B{C{latlonh0}} or C{abs(B{lat0})} exceeds 90°. @raise TypeError: Invalid B{C{ecef}}, not L{EcefKarney}. ''' _TypeError(EcefKarney, ecef=ecef) self._ecef = ecef self.reset(latlonh0, lon0, height0, name=name) @property_RO def ecef(self): '''Get the ECEF converter (L{EcefKarney}). ''' return self._ecef def forward(self, latlonh, lon=None, height=0, M=False): '''Convert from geodetic C{(lat, lon, height)} to local cartesian C{(x, y, z)}. @param latlonh: Either a C{LatLon}, an L{Ecef9Tuple} or C{scalar} latitude in C{degrees}. @keyword lon: Optional C{scalar} longitude in C{degrees} for C{scalar} B{C{latlonh}}. @keyword height: Optional height in C{meter}, vertically above (or below) the surface of the ellipsoid. @keyword M: Optionally, return the rotation L{EcefMatrix} (C{bool}). @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geocentric C{(x, y, z)} coordinates for the given geodetic ones C{(lat, lon, height)}, case C{C} 0, optional L{EcefMatrix} C{M} and C{datum} if available. @raise EcefError: If B{C{latlonh}} not C{LatLon}, L{Ecef9Tuple} or C{scalar} or B{C{lon}} not C{scalar} for C{scalar} B{C{latlonh}} or C{abs(B{lat})} exceeds 90°. @see: Note at method L{EcefKarney.forward}. ''' lat, lon, h, name = _llhn4(latlonh, lon, height, '') t = self.ecef.forward(lat, lon, h, M=M) x, y, z = self.M.rotate(t[:3], *self._t0[:3]) # .x, .y, .z m = self.M.multiply(t.M) if M else None r = Ecef9Tuple(x, y, z, t.lat, t.lon, t.height, 0, m, self.ecef.datum) return self._xnamed(r, name) @property_RO def height0(self): '''Get origin's height (C{meter}). ''' return self._t0.height @property_RO def lat0(self): '''Get origin's latitude (C{degrees}). ''' return self._t0.lat @property_RO def lon0(self): '''Get origin's longitude (C{degrees}). ''' return self._t0.lon @property_RO def M(self): '''Get the rotation matrix (C{EcefMatrix}). ''' return self._t0.M def reset(self, latlonh0=0, lon0=0, height0=0, name=''): '''Reset the local cartesian origin. @keyword latlonh0: Either a C{LatLon}, an L{Ecef9Tuple} or C{scalar} latitude in C{degrees} of the cartesian origin. @keyword lon0: Optional, C{scalar} longitude of the cartesian origin in C{degrees} for C{scalar} B{C{latlonh0}}. @keyword height0: Optional, height of the cartesian origin in C{meter}, vertically above (or below) the surface of the ellipsoid. @keyword name: Optional, new name (C{str}). @raise EcefError: If B{C{latlonh0}} not C{LatLon}, L{Ecef9Tuple} or C{scalar} or B{C{lon0}} not C{scalar} for C{scalar} B{C{latlonh0}} or C{abs(B{lat})} exceeds 90°. ''' lat0, lon0, height0, n = _llhn4(latlonh0, lon0, height0, '0') if name or n: self.ecef.name = self.name = name or n self._t0 = self.ecef.forward(lat0, lon0, height0, M=True) def reverse(self, xyz, y=None, z=None, M=False): '''Convert from local cartesian C{(x, y, z)} to geodetic C{(lat, lon, height)}. @param xyz: Either an L{Ecef9Tuple}, an C{(x, y, z)} 3-tuple or C{scalar} local cartesian C{x} coordinate in C{meter}. @keyword y: Local cartesian C{y} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{z}}. @keyword z: Local cartesian C{z} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{y}}. @keyword M: Optionally, return the rotation L{EcefMatrix} (C{bool}). @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geodetic coordinates C{(lat, lon, height)} for the given geocentric ones C{(x, y, z)}, case C{C}, optional L{EcefMatrix} C{M} and C{datum} if available. @raise EcefError: If B{C{xyz}} not L{Ecef9Tuple} or C{scalar} C{x} or B{C{y}} and/or B{C{z}} not C{scalar} for C{scalar} B{C{xyz}}. @see: Note at method L{EcefKarney.reverse}. ''' xyz_n = _xyzn4(xyz, y, z, Error=EcefError) x, y, z = self.M.unrotate(xyz_n[:3], *self._t0[:3]) # .x, .y, .z t = self.ecef.reverse(x, y, z, M=M) m = self.M.multiply(t.M) if M else None r = Ecef9Tuple(x, y, z, t.lat, t.lon, t.height, t.C, m, self.ecef.datum) return self._xnamed(r, xyz_n[3]) def toStr(self, prec=9): # PYCHOK signature '''Return this L{EcefCartesian} as a string. @keyword prec: Optional precision, number of decimal digits (0..9). @return: This L{EcefCartesian} representation (C{str}). ''' return self.attrs('lat0', 'lon0', 'height0', 'M', 'ecef', 'name', prec=prec) class EcefMatrix(_NamedTuple): '''A rotation matrix. ''' _Names_ = ('_0_0', '_0_1', '_0_2', # row-order '_1_0', '_1_1', '_1_2', '_2_0', '_2_1', '_2_2') def __new__(cls, sa, ca, sb, cb, *_m): '''New L{EcefMatrix} matrix. @param sa: C{sin(phi)} (C{float}). @param ca: C{cos(phi)} (C{float}). @param sb: C{sin(lambda)} (C{float}). @param cb: C{cos(lambda)} (C{float}). @param _m: (INTERNAL) from C{.multiply}. @raise EcefError: If B{C{sa}}, B{C{ca}}, B{C{sb}} or B{C{cb}} outside M{[-1.0, +1.0]}. ''' t = sa, ca, sb, cb if _m: # all 9 matrix elements ... t += _m # ... from .multiply elif max(map(abs, t)) > 1: raise EcefError('%s invalid: %r' % ('sa, ca, sb or cb', t)) else: # build matrix t = (-sb, -cb * sa, cb * ca, cb, -sb * sa, sb * ca, 0, ca, sa) return _NamedTuple.__new__(cls, *t) def copy(self, **unused): # PYCHOK signature '''Make a shallow or deep copy of this instance. @return: The copy (C{This class} or subclass thereof). ''' return _xnamed(self.classof(*self), self.name) __copy__ = __deepcopy__ = copy def multiply(self, other): '''Matrix multiply M{M0' ⋅ M} this matrix transposed with an other matrix. @param other: The other matrix (L{EcefMatrix}). @return: The matrix product (L{EcefMatrix}). @raise TypeError: If B{C{other}} is not L{EcefMatrix}. ''' _TypeError(EcefMatrix, other=other) # like LocalCartesian.MatrixMultiply, transposed(self) x other # <https://GeographicLib.SourceForge.io/html/LocalCartesian_8cpp_source.html> M = (fdot(self[r::3], *other[c::3]) for r in range(3) for c in range(3)) return EcefMatrix(*M) def rotate(self, xyz, *xyz0): '''Forward rotation M{M0' ⋅ ([x, y, z] - [x0, y0, z0])'}. @param xyz: Local C{(x, y, z)} coordinates (C{3-tuple}). @param xyz0: Optional, local C{(x0, y0, z0)} origin (C{3-tuple}). @return: Rotated C{(x, y, z)} location (C{3-tuple}). ''' if xyz0: # and len(xyz) == len(xyz0) xyz = tuple(c - c0 for c, c0 in zip(xyz, xyz0)) # x' = M[0] * x + M[3] * y + M[6] * z # y' = M[1] * x + M[4] * y + M[7] * z # z' = M[2] * x + M[5] * y + M[8] * z return (fdot(self[0::3], *xyz), fdot(self[1::3], *xyz), fdot(self[2::3], *xyz)) def unrotate(self, xyz, *xyz0): '''Inverse rotation M{[x0, y0, z0] + M0 ⋅ [x,y,z]'}. @param xyz: Local C{(x, y, z)} coordinates (C{3-tuple}). @param xyz0: Optional, local C{(x0, y0, z0)} origin (C{3-tuple}). @return: Unrotated C{(x, y, z)} location (C{3-tuple}). ''' # x' = x0 + M[0] * x + M[1] * y + M[2] * z # y' = y0 + M[3] * x + M[4] * y + M[5] * z # z' = z0 + M[6] * x + M[7] * y + M[8] * z xyz = (fdot(self[0:3], *xyz), fdot(self[3:6], *xyz), fdot(self[6:], *xyz)) if xyz0: # and len(xyz) == len(xyz0) xyz = tuple(c0 + c for c0, c in zip(xyz0, xyz)) return xyz class Ecef9Tuple(_NamedTuple): # .ecef.py '''9-Tuple C{(x, y, z, lat, lon, height, C, M, datum)} with geocentric coordinates C{x}, C{y} and C{z}, geodetic coordinates C{lat}, C{lon} and C{height}, case C{C} and optionally, the L{EcefMatrix} C{M} and C{datum}, with C{lat} and C{lon} in C{degrees} and C{x}, C{y}, C{z} and C{height} in C{meter}, usually. ''' _Names_ = ('x', 'y', 'z', 'lat', 'lon', 'height', 'C', 'M', 'datum') @property_RO def lam(self): '''Get the (geodetic) longitude in C{radians} (C{float}). ''' return self.philam.lam @property_RO def latlon(self): '''Get the (geodetic) lat-, longitude in C{degrees} (L{LatLon2Tuple}C{(lat, lon)}). ''' return self._xnamed(LatLon2Tuple(self.lat, self.lon)) @property_RO def latlonheight(self): '''Get the (geodetic) lat-, longitude in C{degrees} and height (L{LatLon3Tuple}C{(lat, lon, height)}). ''' return self._xnamed(self.latlon.to3Tuple(self.height)) @property_RO def latlonheightdatum(self): '''Get the (geodetic) lat-, longitude in C{degrees} with height and datum (L{LatLon4Tuple}C{(lat, lon, height, datum)}). ''' return self._xnamed(self.latlon.to3Tuple(self.height).to4Tuple(self.datum)) @property_RO def phi(self): '''Get the (geodetic) latitude in C{radians} (C{float}). ''' return self.philam.phi @property_RO def philam(self): '''Get the (geodetic) lat-, longitude in C{radians} (L{PhiLam2Tuple}C{(phi, lam)}). ''' return self._xnamed(PhiLam2Tuple(radians(self.lat), radians(self.lon))) @property_RO def philamheight(self): '''Get the (geodetic) lat-, longitude in C{radians} and height (L{PhiLam3Tuple}C{(phi, lam, height)}). ''' return self._xnamed(self.philam.to3Tuple(self.height)) @property_RO def philamheightdatum(self): '''Get the (geodetic) lat-, longitude in C{radians} with height and datum (L{PhiLam4Tuple}C{(phi, lam, height, datum)}). ''' return self._xnamed(self.philam.to3Tuple(self.height).to4Tuple(self.datum)) def toCartesian(self, Cartesian): '''Return the geocentric C{(x, y, z)} coordinates as an ellipsoidal or spherical C{Cartesian}. @param Cartesian: L{ellipsoidalKarney.Cartesian}, L{ellipsoidalNvector.Cartesian}, L{ellipsoidalVincenty.Cartesian}, L{sphericalNvector.Cartesian} or L{sphericalTrigonometry.Cartesian} (sub-)class to return C{(x, y, z)}. @return: A B{C{Cartesian}}C{(x, y, z)} instance. @raise TypeError: Invalid B{C{Cartesian}}. ''' from pygeodesy.cartesianBase import CartesianBase as _CB if not issubclass(Cartesian, _CB): raise _IsNotError(_CB.__name__, Cartesian=Cartesian) r = Cartesian(self) return self._xnamed(r) def toLatLon(self, LatLon=None): '''Return the geodetic C{(lat, lon, height[, datum])} coordinates. @keyword LatLon: Optional (sub-)class to return C{(lat, lon, height[, datum])} or C{None}. @return: An instance of C{LatLon}C{(lat, lon, height[, datum])} if B{C{LatLon}} is not C{None} or a L{LatLon3Tuple}C{(lat, lon, height)} or a L{LatLon4Tuple}C{(lat, lon, height, datum)} if C{datum} is unavailable respectively available. ''' lat, lon = self.latlon # PYCHOK expected h, d = self.height, self.datum # PYCHOK expected if d is None: r = LatLon3Tuple(lat, lon, h) if LatLon is None else \ LatLon(lat, lon, h) elif isinstance(d, Datum): r = LatLon4Tuple(lat, lon, h, d) if LatLon is None else \ LatLon(lat, lon, height=h, datum=d) else: raise AssertionError('%r.%s: %r' % (self, 'datum', d)) return self._xnamed(r) def toVector(self, Vector=None, **kwds): '''Return the geocentric C{(x, y, z)} coordinates as vector. @keyword Vector: Optional vector (sub-)class to return C{(x, y, z)} or C{None}. @keyword kwds: Optional, additional B{C{Vector}} keyword arguments, ignored if C{B{Vector}=None}. @return: A C{Vector}C{(x, y, z, **kwds)} instance or a L{Vector3Tuple}C{(x, y, z)} if B{C{Vector}} is C{None}. @see: Propertes C{xyz} and C{xyzh} ''' return self.xyz if Vector is None else \ self._xnamed(Vector(self.x, self.y, self.z, **kwds)) # PYCHOK x, y, z @property_RO def xyz(self): '''Get the geocentric C{(x, y, z)} coordinates (L{Vector3Tuple}C{(x, y, z)}). ''' return self._xnamed(Vector3Tuple(self.x, self.y, self.z)) @property_RO def xyzh(self): '''Get the geocentric C{(x, y, z)} coordinates and height (L{Vector4Tuple}C{(x, y, z, h)}) ''' return self._xnamed(self.xyz.to4Tuple(self.height)) class EcefVeness(_EcefBase): '''Conversion between geodetic and geocentric, aka I{Earth-Centered, Earth-Fixed} (ECEF) coordinates transcribed from I{Chris Veness}' JavaScript classes U{LatLonEllipsoidal, Cartesian <https://www.Movable-Type.co.UK/scripts/geodesy/docs/latlon-ellipsoidal.js.html>}. @see: U{A Guide to Coordinate Systems in Great Britain <https://www.OrdnanceSurvey.co.UK/documents/resources/guide-coordinate-systems-great-britain.pdf>}, section I{B) Converting between 3D Cartesian and ellipsoidal latitude, longitude and height coordinates}. ''' def __init__(self, a_ellipsoid, f=None, name=''): '''New L{EcefVeness} converter. @param a_ellipsoid: An ellipsoid (L{Ellipsoid}), a datum (L{Datum}) or C{scalar} for the major, equatorial radius of the ellipsoid (C{meter}). @keyword f: C{None} or the ellipsoid flattening (C{scalar}), required for C{scalar} B{C{a_datum_ellipsoid}}, B{C{f}}=0 represents a sphere, negative B{C{f}} a prolate ellipsoid. @keyword name: Optional name (C{str}). @raise EcefError: If B{C{a_ellipsoid}} not L{Ellipsoid}, L{Datum} or C{scalar} or B{C{f}} not C{scalar} or if C{scalar} B{C{a_ellipsoid}} not positive or B{C{f}} not less than 1.0. ''' _EcefBase.__init__(self, a_ellipsoid, f, name) def forward(self, latlonh, lon=None, height=0, M=False): '''Convert from geodetic C{(lat, lon, height)} to geocentric C{(x, y, z)}. @param latlonh: Either a C{LatLon}, an L{Ecef9Tuple} or C{scalar} latitude in C{degrees}. @keyword lon: Optional C{scalar} longitude in C{degrees} for C{scalar} B{C{latlonh}}. @keyword height: Optional height in C{meter}, vertically above (or below) the surface of the ellipsoid. @keyword M: Optionally, return the rotation L{EcefMatrix} (C{bool}). @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geocentric C{(x, y, z)} coordinates for the given geodetic ones C{(lat, lon, height)}, case C{C} 0, L{EcefMatrix} C{M} and C{datum} if available. @raise EcefError: If B{C{latlonh}} not C{LatLon}, L{Ecef9Tuple} or C{scalar} or B{C{lon}} not C{scalar} for C{scalar} B{C{latlonh}} or C{abs(B{lat})} exceeds 90°. ''' lat, lon, h, name = _llhn4(latlonh, lon, height, '') sa, ca, sb, cb = sincos2d(lat, lon) E = self.ellipsoid # radius of curvature in prime vertical t = E.e2s2(sa) # r, _ = E.roc2_(sa, 1) r = 0 if t < EPS else (E.a if t > EPS1 else (E.a / sqrt(t))) x = (h + r) * ca z = (h + r * E.e12) * sa m = self._Matrix(sa, ca, sb, cb) if M else None r = Ecef9Tuple(x * cb, x * sb, z, lat, lon, h, 0, m, self.datum) return self._xnamed(r, name) def reverse(self, xyz, y=None, z=None, **no_M): # PYCHOK unused M '''Convert from geocentric C{(x, y, z)} to geodetic C{(lat, lon, height)} transcribed from I{Chris Veness}' U{JavaScript <https://www.Movable-Type.co.UK/scripts/geodesy/docs/latlon-ellipsoidal.js.html>}. Uses B. R. Bowring’s formulation for μm precision in concise form: U{'The accuracy of geodetic latitude and height equations' <https://www.ResearchGate.net/publication/ 233668213_The_Accuracy_of_Geodetic_Latitude_and_Height_Equations>}, Survey Review, Vol 28, 218, Oct 1985. @param xyz: Either an L{Ecef9Tuple}, an C{(x, y, z)} 3-tuple or C{scalar} ECEF C{x} coordinate in C{meter}. @keyword y: ECEF C{y} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{z}}. @keyword z: ECEF C{z} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{y}}. @keyword no_M: Rotation matrix C{M} not available. @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geodetic coordinates C{(lat, lon, height)} for the given geocentric ones C{(x, y, z)}, case C{C}, L{EcefMatrix} C{M} always C{None} and C{datum} if available. @raise EcefError: If B{C{xyz}} not L{Ecef9Tuple} or C{scalar} C{x} or B{C{y}} and/or B{C{z}} not C{scalar} for C{scalar} B{C{xyz}}. @see: Ralph M. Toms U{'An Efficient Algorithm for Geocentric to Geodetic Coordinate Conversion'<https://www.OSTI.gov/scitech/biblio/110235>}, Sept 1995 and U{'An Improved Algorithm for Geocentric to Geodetic Coordinate Conversion'<https://www.OSTI.gov/scitech/servlets/purl/231228>}, Apr 1996, both from Lawrence Livermore National Laboratory (LLNL). ''' x, y, z, name = _xyzn4(xyz, y, z, Error=EcefError) E = self.ellipsoid p = hypot(x, y) # distance from minor axis r = hypot(p, z) # polar radius if min(p, r) > EPS: # parametric latitude (Bowring eqn 17, replaced) t = (E.b * z) / (E.a * p) * (1 + E.e22 * E.b / r) c = 1 / hypot1(t) s = t * c # geodetic latitude (Bowring eqn 18) a = atan2(z + E.e22 * E.b * s**3, p - E.e2 * E.a * c**3) b = atan2(y, x) # ... and longitude # height above ellipsoid (Bowring eqn 7) sa, ca = sincos2(a) # r = E.a / E.e2s(sa) # length of normal terminated by minor axis # h = p * ca + z * sa - (E.a * E.a / r) h = fsum_(p * ca, z * sa, -E.a * E.e2s(sa)) C, lat, lon = 1, degrees90(a), degrees180(b) # see <https://GIS.StackExchange.com/questions/28446> elif p > EPS: # lat arbitrarily zero C, lat, lon, h = 2, 0.0, degrees180(atan2(y, x)), p - E.a else: # polar lat, lon arbitrarily zero C, lat, lon, h = 3, copysign(90.0, z), 0.0, abs(z) - E.b r = Ecef9Tuple(x, y, z, lat, lon, h, C, None, self.datum) return self._xnamed(r, name) class EcefYou(_EcefBase): '''Conversion between geodetic and geocentric, aka I{Earth-Centered, Earth-Fixed} (ECEF) coordinates using I{Rey-Jer You}'s U{transformations <https://www.ResearchGate.net/publication/240359424>}. @see: W.E. Featherstone, S.J. (Sten) Claessens U{Closed-form transformation between geodetic and ellipsoidal coordinates <https://espace.Curtin.edu.AU/bitstream/handle/20.500.11937/11589/115114_9021_geod2ellip_final.pdf>} Studia Geophysica et Geodaetica, 2008, 52, 1-18 and U{PyMap3D <https://PyPI.org/project/pymap3d>}. ''' def __init__(self, a_ellipsoid, f=None, name=''): '''New L{EcefYou} converter. @param a_ellipsoid: An ellipsoid (L{Ellipsoid}), a datum (L{Datum}) or C{scalar} for the major, equatorial radius of the ellipsoid (C{meter}). @keyword f: C{None} or the ellipsoid flattening (C{scalar}), required for C{scalar} B{C{a_datum_ellipsoid}}, B{C{f}}=0 represents a sphere, negative B{C{f}} a prolate ellipsoid. @keyword name: Optional name (C{str}). @raise EcefError: If B{C{a_ellipsoid}} not L{Ellipsoid}, L{Datum} or C{scalar} or B{C{f}} not C{scalar} or if C{scalar} B{C{a_ellipsoid}} not positive or B{C{f}} not less than 1.0. ''' _EcefBase.__init__(self, a_ellipsoid, f, name) def forward(self, latlonh, lon=None, height=0, M=False): '''Convert from geodetic C{(lat, lon, height)} to geocentric C{(x, y, z)}. @param latlonh: Either a C{LatLon}, an L{Ecef9Tuple} or C{scalar} latitude in C{degrees}. @keyword lon: Optional C{scalar} longitude in C{degrees} for C{scalar} B{C{latlonh}}. @keyword height: Optional height in C{meter}, vertically above (or below) the surface of the ellipsoid. @keyword M: Optionally, return the rotation L{EcefMatrix} (C{bool}). @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geocentric C{(x, y, z)} coordinates for the given geodetic ones C{(lat, lon, height)}, case C{C} 0, L{EcefMatrix} C{M} and C{datum} if available. @raise EcefError: If B{C{latlonh}} not C{LatLon}, L{Ecef9Tuple} or C{scalar} or B{C{lon}} not C{scalar} for C{scalar} B{C{latlonh}} or C{abs(B{lat})} exceeds 90°. ''' lat, lon, h, name = _llhn4(latlonh, lon, height, '') sa, ca, sb, cb = sincos2d(lat, lon) E = self.ellipsoid n = 1.0 / hypot(E.a * ca, E.b * sa) z = (n * E.b2 + h) * sa x = (n * E.a2 + h) * ca m = self._Matrix(sa, ca, sb, cb) if M else None r = Ecef9Tuple(x * cb, x * sb, z, lat, lon, h, 0, m, self.datum) return self._xnamed(r, name) def reverse(self, xyz, y=None, z=None, **no_M): # PYCHOK unused M '''Convert from geocentric C{(x, y, z)} to geodetic C{(lat, lon, height)} using I{Rey-Jer You}'s transformation. @param xyz: Either an L{Ecef9Tuple}, an C{(x, y, z)} 3-tuple or C{scalar} ECEF C{x} coordinate in C{meter}. @keyword y: ECEF C{y} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{z}}. @keyword z: ECEF C{z} coordinate in C{meter} for C{scalar} B{C{xyz}} and B{C{y}}. @keyword no_M: Rotation matrix C{M} not available. @return: An L{Ecef9Tuple}C{(x, y, z, lat, lon, height, C, M, datum)} with geodetic coordinates C{(lat, lon, height)} for the given geocentric ones C{(x, y, z)}, case C{C} 1, L{EcefMatrix} C{M} always C{None} and C{datum} if available. @raise EcefError: If B{C{xyz}} not L{Ecef9Tuple} or C{scalar} C{x} or B{C{y}} and/or B{C{z}} not C{scalar} for C{scalar} B{C{xyz}}. ''' x, y, z, name = _xyzn4(xyz, y, z, Error=EcefError) x2, y2, z2 = x**2, y**2, z**2 r2 = fsum_(x2, y2, z2) # = hypot3(x2, y2, z2)**2 E = self.ellipsoid e = sqrt(E.a2 - E.b2) e2 = e**2 u = sqrt(fsum_(r2, -e2, hypot(r2 - e2, 2 * e * z)) / 2) p = hypot(u, e) q = hypot(x, y) B = atan2(p * z, u * q) # beta0 = atan(p / u * z / q) sB, cB = sincos2(B) p *= E.a B += fsum_(u * E.b, -p, e2) * sB / (p / cB - e2 * cB) sB, cB = sincos2(B) h = hypot(z - E.b * sB, q - E.a * cB) if fsum_(x2, y2, z2 * E.a_b**2) < E.a2: h = -h # inside ellipsoid r = Ecef9Tuple(x, y, z, degrees(atan2(E.a * sB, E.b * cB)), # atan(E.a_b * tan(B)) degrees(atan2(y, x)), h, 1, None, self.datum) return self._xnamed(r, name) # **) MIT License # # Copyright (C) 2016-2020 -- mrJean1 at Gmail -- All Rights Reserved. # # Permission is hereby granted, free of charge, to any person obtaining a # copy of this software and associated documentation files (the "Software"), # to deal in the Software without restriction, including without limitation # the rights to use, copy, modify, merge, publish, distribute, sublicense, # and/or sell copies of the Software, and to permit persons to whom the # Software is furnished to do so, subject to the following conditions: # # The above copyright notice and this permission notice shall be included # in all copies or substantial portions of the Software. # # THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS # OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, # FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL # THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR # OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, # ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR # OTHER DEALINGS IN THE SOFTWARE.