| 1 | #include "slalib.h"
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| 2 | #include "slamac.h"
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| 3 | float slaRvlsrd ( float r2000, float d2000 )
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| 4 | /*
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| 5 | ** - - - - - - - - - -
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| 6 | ** s l a R v l s r d
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| 7 | ** - - - - - - - - - -
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| 8 | **
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| 9 | ** Velocity component in a given direction due to the Sun's
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| 10 | ** motion with respect to the dynamical Local Standard of Rest.
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| 11 | **
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| 12 | ** (single precision)
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| 13 | **
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| 14 | ** Given:
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| 15 | ** r2000,d2000 float J2000.0 mean RA,Dec (radians)
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| 16 | **
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| 17 | ** Result:
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| 18 | ** Component of "peculiar" solar motion in direction R2000,D2000 (km/s)
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| 19 | **
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| 20 | ** Sign convention:
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| 21 | ** The result is +ve when the Sun is receding from the given point on
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| 22 | ** the sky.
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| 23 | **
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| 24 | ** Note: The Local Standard of Rest used here is the "dynamical" LSR,
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| 25 | ** a point in the vicinity of the Sun which is in a circular
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| 26 | ** orbit around the Galactic centre. The Sun's motion with
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| 27 | ** respect to the dynamical LSR is called the "peculiar" solar
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| 28 | ** motion.
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| 29 | **
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| 30 | ** There is another type of LSR, called a "kinematical" LSR. A
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| 31 | ** kinematical LSR is the mean standard of rest of specified star
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| 32 | ** catalogues or stellar populations, and several slightly
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| 33 | ** different kinematical LSRs are in use. The Sun's motion with
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| 34 | ** respect to an agreed kinematical LSR is known as the "standard"
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| 35 | ** solar motion. To obtain a radial velocity correction with
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| 36 | ** respect to an adopted kinematical LSR use the routine slaRvlsrk.
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| 37 | **
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| 38 | ** Reference: Delhaye (1965), in "Stars and Stellar Systems", vol 5, p73.
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| 39 | **
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| 40 | ** Called: slaCs2c, slaVdv
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| 41 | **
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| 42 | ** Last revision: 11 March 1994
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| 43 | **
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| 44 | ** Copyright P.T.Wallace. All rights reserved.
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| 45 | */
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| 46 | {
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| 47 | /*
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| 48 | ** Peculiar solar motion from Delhaye 1965: in Galactic Cartesian
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| 49 | ** coordinates (+9,+12,+7) km/s. This corresponds to about 16.6 km/s
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| 50 | ** towards Galactic coordinates L2 = 53 deg, B2 = +25 deg, or RA,Dec
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| 51 | ** 17 49 58.7 +28 07 04 J2000.
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| 52 | **
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| 53 | ** The solar motion is expressed here in the form of a J2000.0
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| 54 | ** equatorial Cartesian vector:
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| 55 | **
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| 56 | ** va(1) = x = -speed*cos(ra)*cos(dec)
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| 57 | ** va(2) = y = -speed*sin(ra)*cos(dec)
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| 58 | ** va(3) = z = -speed*sin(dec)
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| 59 | */
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| 60 | static float va[3] = { 0.63823f, 14.58542f, -7.80116f };
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| 61 | float vb[3];
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| 62 |
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| 63 | /* Convert given J2000 RA,dec to x,y,z */
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| 64 | slaCs2c ( r2000, d2000, vb );
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| 65 |
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| 66 | /* Compute dot product with solar motion vector */
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| 67 | return slaVdv ( va, vb );
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| 68 | }
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