SUBROUTINE iau_ATOIQ ( TYPE, OB1, OB2, ASTROM, RI, DI ) *+ * - - - - - - - - - - * i a u _ A T O I Q * - - - - - - - - - - * * Quick observed place to CIRS, given the star-independent astrometry * parameters. * * Use of this routine is appropriate when efficiency is important and * where many star positions are all to be transformed for one date. * The star-independent astrometry parameters can be obtained by calling * iau_APIO[13] or iau_APCO[13]. * * Status: support routine. * * Given: * TYPE c*(*) type of coordinates: 'R', 'H' or 'A' (Note 2) * OB1 d observed Az, HA or RA (radians; Az is N=0,E=90) * OB2 d observed ZD or Dec (radians) * ASTROM d(30) star-independent astrometry parameters: * (1) PM time interval (SSB, Julian years) * (2-4) SSB to observer (vector, au) * (5-7) Sun to observer (unit vector) * (8) distance from Sun to observer (au) * (9-11) v: barycentric observer velocity (vector, c) * (12) sqrt(1-|v|^2): reciprocal of Lorenz factor * (13-21) bias-precession-nutation matrix * (22) longitude + s' (radians) * (23) polar motion xp wrt local meridian (radians) * (24) polar motion yp wrt local meridian (radians) * (25) sine of geodetic latitude * (26) cosine of geodetic latitude * (27) magnitude of diurnal aberration vector * (28) "local" Earth rotation angle (radians) * (29) refraction constant A (radians) * (30) refraction constant B (radians) * * Returned: * RI d CIRS right ascension (CIO-based, radians) * DI d CIRS declination (radians) * * Notes: * * 1) "Observed" Az,ZD means the position that would be seen by a * perfect geodetically aligned theodolite. This is related to the * observed HA,Dec via the standard rotation, using the geodetic * latitude (corrected for polar motion), while the observed HA and * (CIO-based) RA are related simply through the Earth rotation angle * and the site longitude. "Observed" RA,Dec or HA,Dec thus means * the position that would be seen by a perfect equatorial with its * polar axis aligned to the Earth's axis of rotation. * * 2) Only the first character of the type argument is significant. * 'R' or 'r' indicates that OB1 and OB2 are the observed right * ascension (CIO-based) and declination; 'H' or 'h' indicates that * they are hour angle (west +ve) and declination; anything else * ('A' or 'a' is recommended) indicates that OB1 and OB2 are * azimuth (north zero, east 90 deg) and zenith distance. (Zenith * distance is used rather than altitude in order to reflect the * fact that no allowance is made for depression of the horizon.) * * 3) The accuracy of the result is limited by the corrections for * refraction, which use a simple A*tan(z) + B*tan^3(z) model. * Providing the meteorological parameters are known accurately and * there are no gross local effects, the predicted intermediate * coordinates should be within 0.5 arcsec (optical) or 1 arcsec * (radio) for a zenith distance of less than 75 degrees, better * than 30 arcsec (optical or radio) at 85 degrees and better than * 20 arcmin (optical) or 25 arcmin (radio) at the horizon. * * Without refraction, the complementary routines iau_ATIOQ and * iau_ATOIQ are self-consistent to better than 1 microarcsecond all * over the celestial sphere. With refraction included, consistency * falls off at high zenith distances, but is still better than * 0.05 arcsec at 85 degrees. * * 4) It is advisable to take great care with units, as even unlikely * values of the input parameters are accepted and processed in * accordance with the models used. * * 5) The star-independent astrometry parameters in ASTROM may be * computed with iau_APIO13 (or iau_APIO). If nothing has changed * significantly except the time, iau_APER13 (or iau_APER) may be * used to perform the requisite adjustment to the ASTROM array. * * Called: * iau_S2C spherical coordinates to unit vector * iau_C2S p-vector to spherical * iau_ANP normalize angle into range 0 to 2pi * * This revision: 2022 August 30 * * SOFA release 2023-10-11 * * Copyright (C) 2023 IAU SOFA Board. See notes at end. * *----------------------------------------------------------------------- IMPLICIT NONE CHARACTER*(*) TYPE DOUBLE PRECISION OB1, OB2, ASTROM(30), RI, DI * Minimum sine of altitude for refraction purposes DOUBLE PRECISION SELMIN PARAMETER ( SELMIN = 0.05D0 ) CHARACTER C DOUBLE PRECISION C1, C2, SPHI, CPHI, CE, XAEO, YAEO, ZAEO, V(3), : XMHDO, YMHDO, ZMHDO, AZ, SZ, ZDO, REFA, REFB, : TZ, DREF, ZDT, XAET, YAET, ZAET, : XMHDA, YMHDA, ZMHDA, F, XHD, YHD, ZHD, : SX, CX, SY, CY, HMA DOUBLE PRECISION iau_ANP * - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - * Coordinate type. C = TYPE(:1) * Coordinates. C1 = OB1 C2 = OB2 * Sin, cos of latitude. SPHI = ASTROM(25) CPHI = ASTROM(26) * Standardize coordinate type. IF ( C.EQ.'r' .OR. C.EQ.'R' ) THEN C = 'R' ELSE IF ( C.EQ.'h' .OR. C.EQ.'H' ) THEN C = 'H' ELSE C = 'A' END IF * If Az,ZD, convert to Cartesian (S=0,E=90). IF ( C.EQ.'A' ) THEN CE = SIN(C2) XAEO = - COS(C1) * CE YAEO = SIN(C1) * CE ZAEO = COS(C2) ELSE * If RA,Dec, convert to HA,Dec. IF ( C.EQ.'R' ) C1 = ASTROM(28) - C1 * To Cartesian -HA,DeC. CALL iau_S2C ( -C1, C2, V ) XMHDO = V(1) YMHDO = V(2) ZMHDO = V(3) * To Cartesian Az,El (S=0,E=90). XAEO = SPHI*XMHDO - CPHI*ZMHDO YAEO = YMHDO ZAEO = CPHI*XMHDO + SPHI*ZMHDO END IF * Azimuth (S=0,E=90). IF ( XAEO.NE.0D0 .OR. YAEO.NE.0D0 ) THEN AZ = ATAN2(YAEO,XAEO) ELSE AZ = 0D0 END IF * Sine of observed ZD, and observed ZD. SZ = SQRT ( XAEO*XAEO + YAEO*YAEO ) ZDO = ATAN2 ( SZ, ZAEO ) * * Refraction * ---------- * Fast algorithm using two constant model. REFA = ASTROM(29) REFB = ASTROM(30) ZAEO = MAX ( ZAEO, SELMIN ) TZ = SZ / ZAEO DREF = ( REFA + REFB*TZ*TZ ) * TZ ZDT = ZDO + DREF * To Cartesian Az,ZD. CE = SIN(ZDT) XAET = COS(AZ) * CE YAET = SIN(AZ) * CE ZAET = COS(ZDT) * Cartesian Az,ZD to Cartesian -HA,DeC. XMHDA = SPHI*XAET + CPHI*ZAET YMHDA = YAET ZMHDA = - CPHI*XAET + SPHI*ZAET * Diurnal aberration. F = ( 1D0 + ASTROM(27)*YMHDA ) XHD = F * XMHDA YHD = F * ( YMHDA - ASTROM(27) ) ZHD = F * ZMHDA * Polar motion. SX = SIN(ASTROM(23)) CX = COS(ASTROM(23)) SY = SIN(ASTROM(24)) CY = COS(ASTROM(24)) V(1) = CX*XHD + SX*SY*YHD - SX*CY*ZHD V(2) = CY*YHD + SY*ZHD V(3) = SX*XHD - CX*SY*YHD + CX*CY*ZHD * To spherical -HA,Dec. CALL iau_C2S ( V, HMA, DI ) * Right ascension. RI = iau_ANP ( ASTROM(28) + HMA ) * Finished. *+---------------------------------------------------------------------- * * Copyright (C) 2023 * Standards of Fundamental Astronomy Board * of the International Astronomical Union. * * ===================== * SOFA Software License * ===================== * * NOTICE TO USER: * * BY USING THIS SOFTWARE YOU ACCEPT THE FOLLOWING SIX TERMS AND * CONDITIONS WHICH APPLY TO ITS USE. * * 1. The Software is owned by the IAU SOFA Board ("SOFA"). * * 2. 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