;+ ; computes the projected velocity of the telescope wrt ; six coordinate systems: geo, helio, bary, lsrk, lsrd, gal ; negative velocities mean approach ; ; The standard LSR is defined as follows: the sun moves at 20.0 km/s ; toward ra=18.0h, dec=30.0 deg in 1900 epoch coords ; ;

CHDOPPLER IS NOT VECTORIZED; ONLY SINGLE NUMBERS ; ;

; This code came via e-mail from Carl Heiles via Tom Bania on 11/04/2004. ; Local changes: ;

; ; Previous revision history: carlh 29oct04 ; ; ; @param ra {in}{required} The source ra in decimal hours, equinox 2000 ; @param dec {in}{required} The source dec in decimal hours, equinox 2000 ; @param julday {in}{required} The julian day ; ; @keyword obspos {in}{optional}{double [2]} observatory position ; [East longitude, latitude] in degrees. ; Uses the GBT position if not specified. ; ; @keyword light {in}{optional}{boolean} When set, returns the ; velocity as a fraction of c ; ; ; @returns The velocity in km/s, or as a faction of c if ; the keyword /light is specified. the result is a 6-element ; vector whose elements are [geo, helio, bary, lsrk, lsrd, gal]. ; ; @uses baryvel ; @uses precess ; @uses juldaytolmst ; ; @version $Id: chdoppler.pro,v 1.3 2005/04/08 20:36:06 bgarwood Exp $ ;- function chdoppler, ra, dec, julday, $ obspos=obspos, light=light ; ; Default to GBT if obspos not provided. if (not keyword_set(obspos)) then begin obspos=dblarr(2); obspos[0]=[-(79.D + 50.D/60.D + 23.42D/3600.D)] obspos[1]=[(38.D + 25.D/60.D + 59.26D/3600.D)] endif ;------------------ORBITAL SECTION------------------------- ;GET THE COMPONENTS OF RA AND DEC, 2000u EPOCH rasource=ra*15.d*!dtor decsource=dec*!dtor xxsource = dblarr(3) xxsource[0] = cos(decsource) * cos(rasource) xxsource[1] = cos(decsource) * sin(rasource) xxsource[2] = sin(decsource) ;GET THE EARTH VELOCITY WRT THE SUN CENTER baryvel, julday, 2000.,vvorbit,velb ;PROJECTED VELOCITY OF EARTH CENTER WRT SUN TO THE SOURCE pvorbit_helio = total(vvorbit* xxsource) pvorbit_bary = total(velb* xxsource) ;-----------------------LSRK SECTION------------------------- ;THE STANDARD LSRK IS DEFINED AS FOLLOWS: THE SUN MOVES AT 20.0 KM/S ;TOWARD RA=18.0H, DEC=30.0 DEG IN 1900 EPOCH COORDS ;using PRECESS, this works out to ra=18.063955 dec=30.004661 in 2000 ;coords. ralsrk_rad= 2.d*!pi*18.d/24.d declsrk_rad= !dtor*30.d precess, ralsrk_rad, declsrk_rad, 1900.d, 2000.d,/radian ;FIND THE COMPONENTS OF THE VELOCITY OF THE SUN WRT THE LSRK FRAME xxlsrk = dblarr(3) xxlsrk[0] = cos(declsrk_rad) * cos(ralsrk_rad) xxlsrk[1] = cos(declsrk_rad) * sin(ralsrk_rad) xxlsrk[2] = sin(declsrk_rad) vvlsrk = 20.d*xxlsrk ;PROJECTED VELOCITY OF THE SUN WRT LSRK TO THE SOURCE pvlsrk=total(vvlsrk*xxsource) ;-----------------------LSRD SECTION------------------------- ;THE LSRD IS DEFINED AS FOLLOWS: THE SUN MOVES AT 16.6 KM/S ;TOWARD RA=17:49:58.7 hours, DEC=28.07.04 DEG IN 2000 EPOCH COORDS ralsrd_rad= 2.d*!dpi*(17.D + 49.D/60.D + 58.7D/3600.D)/24.d declsrd_rad= !dtor*(28.D + 07.D/60.D + 04.0D/3600.D) ;FIND THE COMPONENTS OF THE VELOCITY OF THE SUN WRT THE LSRD FRAME xxlsrd = dblarr(3) xxlsrd[0] = cos(declsrd_rad) * cos(ralsrd_rad) xxlsrd[1] = cos(declsrd_rad) * sin(ralsrd_rad) xxlsrd[2] = sin(declsrd_rad) vvlsrd = 16.6D*xxlsrd ;PROJECTED VELOCITY OF THE SUN WRT LSRD TO THE SOURCE pvlsrd=total(vvlsrd*xxsource) ;-----------------------GALACTOCENTRIC SECTION------------------ ; LSRD + 220 km/s towards RA=21:12:01.1 DEC=48.19.47 in J2000 Epoch ragal_rad = 2.d*!dpi*(21.D + 12.D/60.D + 01.1D/3600.D)/24.d decgal_rad = !dtor*(48.D + 19.D/60.D + 47.D/3600.D) ; Find the components of the velocity of the sun wrt this frame xxgal = dblarr(3) xxgal[0] = cos(decgal_rad) * cos(ragal_rad) xxgal[1] = cos(decgal_rad) * sin(ragal_rad) xxgal[2] = sin(decgal_rad) vvgal = 220.D*xxgal ;PROJECTED VELOCITY OF THE SUN WRT GAL TO THE SOURCE pvgal=total(vvgal*xxsource) ;---------------------EARTH SPIN SECTION------------------------ lst_mean= 24.d/(2.d*!pi)*juldaytolmst( julday,obslong=obspos[0]) raspin=(lst_mean- ra- 6.d)* 15.d* !dtor decspin=0.0d*!dtor ;PROJECTED DISTANCE FROM CENTER OF EARTH lat=obspos[1] gclat = lat - 0.1924d * sin(2.d*lat*!dtor) ; true angle lat rearth =( 0.99883d + 0.00167d * cos(2.d*lat*!dtor))* 6378.1d ;dist from center, km rho=rearth*cos(gclat*!dtor) ;SPIN VELOCITY, KM/S vspin=2.d*!pi*rho/86164.090d xxspin = dblarr(3) xxspin[0] = cos(decspin) * cos(raspin) xxspin[1] = cos(decspin) * sin(raspin) xxspin[2] = sin(decspin) vvspin = vspin*xxspin ;PROJECTED VELOCITY OF STATION WRT EARTH CENTER TO SOURCE pvspin=total(vvspin*xxsource) ;---------------------NOW PUT IT ALL TOGETHER------------------ vtotal= dblarr( 6) vtotal[0]= -pvspin vtotal[1]= -shiftvel(pvspin,pvorbit_helio) vtotal[2]= -shiftvel(pvspin,pvorbit_bary) vtotal[3]= -shiftvel(-vtotal[2],pvlsrk) vtotal[4]= -shiftvel(-vtotal[2],pvlsrd) vtotal[5]= -shiftvel(-vtotal[4],pvgal) if keyword_set(light) then vtotal=vtotal/(!gc.light_speed*1.d3) return,vtotal end