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📄 bprecess.pro

📁 basic median filter simulation
💻 PRO
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pro Bprecess, ra, dec, ra_1950, dec_1950, MU_RADEC = mu_radec,  $                  PARALLAX = parallax,  RAD_VEL = rad_vel, EPOCH = epoch;+; NAME:;       BPRECESS; PURPOSE:;       Precess positions from J2000.0 (FK5) to B1950.0 (FK4); EXPLANATION:;       Calculates the mean place of a star at B1950.0 on the FK4 system from;       the mean place at J2000.0 on the FK5 system.    ;; CALLING SEQUENCE:;       bprecess, ra, dec, ra_1950, dec_1950, [ MU_RADEC = , PARALLAX = ;                                       RAD_VEL =, EPOCH =   ];; INPUTS:;       RA,DEC - Input J2000 right ascension and declination in *degrees*.;               Scalar or N element vector;; OUTPUTS:;       RA_1950, DEC_1950 - The corresponding B1950 right ascension and ;               declination in *degrees*.    Same number of elements as;               RA,DEC but always double precision.;; OPTIONAL INPUT-OUTPUT KEYWORDS;       MU_RADEC - 2xN element double precision vector containing the proper ;                  motion in seconds of arc per tropical *century* in right ;                  ascension and declination.;       PARALLAX - N_element vector giving stellar parallax (seconds of arc);       RAD_VEL  - N_element vector giving radial velocity in km/s;;       The values of MU_RADEC, PARALLAX, and RADVEL will all be modified;       upon output to contain the values of these quantities in the;       B1950 system.  The parallax and radial velocity will have a very ;       minor influence on the B1950 position.   ;;       EPOCH - scalar giving epoch of original observations, default 2000.0d;           This keyword value is only used if the MU_RADEC keyword is not set.; NOTES:;       The algorithm is taken from the Explanatory Supplement to the ;       Astronomical Almanac 1992, page 186.;       Also see Aoki et al (1983), A&A, 128,263;;       BPRECESS distinguishes between the following two cases:;       (1) The proper motion is known and non-zero;       (2) the proper motion is unknown or known to be exactly zero (i.e.;               extragalactic radio sources).   In this case, the reverse of ;               the algorithm in Appendix 2 of Aoki et al. (1983) is used to ;               ensure that the output proper motion is  exactly zero. Better ;               precision can be achieved in this case by inputting the EPOCH ;               of the original observations.;;       The error in using the IDL procedure PRECESS for converting between;       B1950 and J1950 can be up to 1.5", mainly in right ascension.   If;       better accuracy than this is needed then BPRECESS should be used.;;       An unsystematic comparison of BPRECESS with the IPAC precession ;       routine (http://nedwww.ipac.caltech.edu/forms/calculator.html) always ;       gives differences less than 0.15".; EXAMPLE:;       The SAO2000 catalogue gives the J2000 position and proper motion for;       the star HD 119288.   Find the B1950 position. ;;       RA(2000) = 13h 42m 12.740s      Dec(2000) = 8d 23' 17.69''  ;       Mu(RA) = -.0257 s/yr      Mu(Dec) = -.090 ''/yr;;       IDL> mu_radec = 100D* [ -15D*.0257, -0.090 ];       IDL> ra = ten(13, 42, 12.740)*15.D ;       IDL> dec = ten(8, 23, 17.69);       IDL> bprecess, ra, dec, ra1950, dec1950, mu_radec = mu_radec;       IDL> print, adstring(ra1950, dec1950,2);               ===> 13h 39m 44.526s    +08d 38' 28.63";; REVISION HISTORY:;       Written,    W. Landsman                October, 1992;       Vectorized, W. Landsman                February, 1994;       Treat case where proper motion not known or exactly zero  November 1994;       Handling of arrays larger than 32767   Lars L. Christensen, march, 1995;       Converted to IDL V5.0   W. Landsman   September 1997;       Fixed bug where A term not initialized for vector input ;            W. Landsman        February 2000;       ;-     On_error,2  if N_params() LT 4 then begin     print,'Syntax - BPRECESS, ra,dec, ra_1950, dec_1950, [MU_RADEC ='      print,'                            PARALLAX = , RAD_VEL = ]'     print,'  Input RA and Dec should be given in DEGREES for J2000'     print,'  Proper motion, MU_RADEC, (optional) in arc seconds per *century*'     print,'  Parallax (optional) in arc seconds'           print,'  Radial Velocity (optional) in km/s'     return  endif  N = N_elements( ra )  if N EQ 0 then message,'ERROR - First parameter (RA vector) is undefined'  if not keyword_set( RAD_VEL) then rad_vel = dblarr(N) else begin        rad_vel = rad_vel*1.        if N_elements( RAD_VEL) NE N then message, $        'ERROR - RAD_VEL keyword vector must contain ' + strtrim(N,2) +' values'  endelse  if keyword_set( MU_RADEC) then begin         if (N_elements( mu_radec) NE 2*N ) then message, $    'ERROR - MU_RADEC keyword (proper motion) be dimensioned (2,' + $                 strtrim(N,2) + ')'        mu_radec = mu_radec*1.  endif  if not keyword_set( Parallax) then parallax = dblarr(N) else $        parallax = parallax*1.  if not keyword_set(Epoch) then epoch = 2000.0d0  radeg = 180.D/!DPI  sec_to_radian = 1.d0/radeg/3600.d0 M =  [ [+0.9999256795D, -0.0111814828D, -0.0048590040D,  $         -0.000551D,  -0.238560D,     +0.435730D     ], $       [ +0.0111814828D, +0.9999374849D, -0.0000271557D,  $          +0.238509D,     -0.002667D,      -0.008541D     ], $       [ +0.0048590039D, -0.0000271771D, +0.9999881946D , $         -0.435614D,      +0.012254D,      +0.002117D      ], $       [ -0.00000242389840D, +0.00000002710544D, +0.00000001177742D, $         +0.99990432D,    -0.01118145D,    -0.00485852D    ], $       [ -0.00000002710544D, -0.00000242392702D, +0.00000000006585D, $         +0.01118145D,     +0.99991613D,    -0.00002716D    ], $       [ -0.00000001177742D, +0.00000000006585D,-0.00000242404995D, $         +0.00485852D,   -0.00002717D,    +0.99996684D] ]  A_dot = 1D-3*[1.244D, -1.579D, -0.660D ]           ;in arc seconds per century ra_rad = ra/radeg       &      dec_rad = dec/radeg cosra =  cos( ra_rad )  &       sinra = sin( ra_rad ) cosdec = cos( dec_rad ) &      sindec = sin( dec_rad ) dec_1950 = dec*0. ra_1950 = ra*0. for i = 0L, N-1 do begin; Following statement moved inside loop in Feb 2000. A = 1D-6*[ -1.62557D, -0.31919D, -0.13843D]        ;in radians r0 = [ cosra[i]*cosdec[i], sinra[i]*cosdec[i], sindec[i] ] if keyword_set(mu_radec) then begin mu_a = mu_radec[ 0, i ] mu_d = mu_radec[ 1, i ] r0_dot = [ -mu_a*sinra[i]*cosdec[i] - mu_d*cosra[i]*sindec[i] , $ ;Velocity vector             mu_a*cosra[i]*cosdec[i] - mu_d*sinra[i]*sindec[i] , $             mu_d*cosdec[i] ] + 21.095d * rad_vel[i] * parallax[i] * r0 endif else r0_dot = [0.0d0, 0.0d0, 0.0d0]  R_0 = [ r0, r0_dot ]  R_1 =  M # R_0 ; Include the effects of the E-terms of aberration to form r and r_dot. r1 = R_1[0:2]   r1_dot = R_1[3:5]  if not keyword_set(Mu_radec) then begin        r1 = r1 + sec_to_radian * r1_dot * (epoch - 1950.0d)/100.        A = A + sec_to_radian * A_dot * (epoch - 1950.0d)/100. endif x1 = R_1[0]   &   y1 = R_1[1]    &  z1 = R_1[2] rmag = sqrt( x1^2 + y1^2 + z1^2 ) s1 = r1/rmag    & s1_dot = r1_dot/rmag s = s1 for j = 0,2 do begin    r = s1 + A - (total(s * A))*s    s = r/rmag endfor  x = r[0]          & y = r[1]     &  z = r[2]   r2 = x^2 + y^2 + z^2 rmag = sqrt( r2 )  if keyword_set(Mu_radec) then begin         r_dot = s1_dot + A_dot - ( total( s * A_dot))*s         x_dot = r_dot[0]  & y_dot= r_dot[1]  &  z_dot = r_dot[2]         mu_radec[0,i] = ( x*y_dot - y*x_dot) / ( x^2 + y^2)         mu_radec[1,i] = ( z_dot* (x^2 + y^2) - z*(x*x_dot + y*y_dot) ) /  $                     ( r2*sqrt( x^2 + y^2) ) endif dec_1950[i] = asin( z / rmag) ra_1950[i] = atan( y, x)  if parallax[i] GT 0. then begin      rad_vel[i] = ( x*x_dot + y*y_dot + z*z_dot )/ (21.095*Parallax[i]*rmag)      parallax[i] = parallax[i] / rmag  endif endfor neg = where( ra_1950 LT 0, NNeg ) if Nneg GT 0 then ra_1950[neg] = ra_1950[neg] + 2.D*!DPI ra_1950 = ra_1950*radeg & dec_1950 = dec_1950*radeg; Make output scalar if input was scalar sz = size(ra) if sz[0] EQ 0 then begin        ra_1950 = ra_1950[0]     &      dec_1950 = dec_1950[0] endif return end

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