13.07.2013 Views

USNO Circular 179 - U.S. Naval Observatory

USNO Circular 179 - U.S. Naval Observatory

USNO Circular 179 - U.S. Naval Observatory

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

ABBREVIATIONS & SYMBOLS xi<br />

GMST Greenwich mean sidereal time 2.3, 2.6.2<br />

GPS Global Positioning System<br />

HCRF Hipparcos Celestial Reference Frame 3.1, 3.4<br />

IAG International Association of Geodesy<br />

IAU International Astronomical Union<br />

ICRF International Celestial Reference Frame 3.1, 3.4<br />

ICRS International Celestial Reference System 3.1, 3.4<br />

IERS International Earth Rotation and Reference System Service<br />

ITRF International Terrestrial Reference Frame 6.4<br />

ITRS International Terrestrial Reference System 6.4, 6.5.2<br />

IUGG International Union of Geodesy and Geophysics<br />

J2000.0 the epoch 2000 January 1, 12h TT (JD 2451545.0 TT) at the geocenter 2.2<br />

(“J2000.0 system” is shorthand for the celestial reference system defined 3.2<br />

by the mean dynamical equator and equinox of J2000.0.)<br />

JD Julian date (time scale used should be specified)<br />

JPL Jet Propulsion Laboratory<br />

mas milliarcsecond (= 10 −3 arcsecond ≈ 4.8×10 −9 radian)<br />

N nutation matrix (for transformation from mean to true system of date) 5.4, 5.4.2<br />

n unit vector toward the CIP (celestial pole) 5.4,6.5.1<br />

NOVAS <strong>Naval</strong> <strong>Observatory</strong> Vector Astrometry Subroutines (software)<br />

P precession matrix (for transformation from J2000.0 system to mean system<br />

of date)<br />

R1(φ) rotation matrix to transform column 3-vectors from one cartesian coordinate<br />

system to another. Final system is formed by rotating original<br />

system about its own x-axis by angle φ (counterclockwise as viewed from<br />

the +x direction):<br />

R1(φ) =<br />

⎛<br />

⎜<br />

⎝<br />

1 0 0<br />

0 cos φ sin φ<br />

0 − sin φ cos φ<br />

R2(φ) rotation matrix to transform column 3-vectors from one cartesian coordinate<br />

system to another. Final system is formed by rotating original<br />

system about its own y-axis by angle φ (counterclockwise as viewed from<br />

the +y direction):<br />

R2(φ) =<br />

⎛<br />

⎜<br />

⎝<br />

cos φ 0 − sin φ<br />

0 1 0<br />

sin φ 0 cos φ<br />

R3(φ) rotation matrix to transform column 3-vectors from one cartesian coordinate<br />

system to another. Final system is formed by rotating original<br />

system about its own z-axis by angle φ (counterclockwise as viewed from<br />

the +z direction):<br />

R3(φ) =<br />

⎛<br />

⎜<br />

⎝<br />

cos φ sin φ 0<br />

− sin φ cos φ 0<br />

0 0 1<br />

⎞<br />

⎟<br />

⎠<br />

⎞<br />

⎟<br />

⎠<br />

⎞<br />

⎟<br />

⎠<br />

5.4, 5.4.2

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!