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courses:ast201:4 [2023/11/01 00:32] – [1.3 Equatorial system] asad | courses:ast201:4 [2023/11/08 21:10] (current) – [2.1 Astronomical Unit (AU)] asad | ||
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The relation between the equatorial and horizon systems is shown above. It assumes an observer located at a latitude of $60$ degrees north on Earth. Both spheres show the horizon, equator and observer' | The relation between the equatorial and horizon systems is shown above. It assumes an observer located at a latitude of $60$ degrees north on Earth. Both spheres show the horizon, equator and observer' | ||
- | Altitude of NCP = Geodetic latitude of observer. | + | The following equations can all be derived geometrically from the above diagram. |
+ | - Altitude of NCP = Geodetic latitude of observer | ||
+ | - Object HA = Meridian RA - Object RA | ||
+ | - Sidereal day = Time between upper meridian transits of the March equinox | ||
+ | - Sidereal time = Object RA on the upper meridian | ||
+ | - Object HA = Sidereal time now - sidereal time when the object culminates | ||
- | Object HA = Meridian RA - Object RA | + | === - Precession and nutation === |
+ | The equatorial system is not inertial, it is accelerated due to the long-term general **precession** and short-term oscillatory **nutation**. | ||
- | Sidereal day = Time between upper meridian transits of the March equinox | + | {{: |
- | Sidereal time = Object RA on the upper meridian | + | As shown above, |
- | Object HA = Sidereal time now - sidereal time when the object culminates | + | NCP completes one orbit in 26,000 years moving at an almost constant speed. So the celestial equator moves at an almost constant speed westward toward ecliptic at a rate of $5029.097$ arcsec (1.4 deg) per century, i. e. almost $50'' |
- | === - Measuring RA-DEC === | + | Hipparchus already knew about precssion. Polaris was not always so close to the NCP. Around 4500 years ago, Thuban was the pole star. After 12,000 years, Vega will be the pole star and Polaris will have a declination of $45$ degrees. |
- | Transit telescope / Meridian circle | + | |
- | {{:courses: | + | {{https:// |
- | {{: | + | Unlike the **lunisolar** precession, **planetary** precession causes the obliquity, i. e. distance between the ecliptic and celestial axes, to change. It results in an oscillation on top of the precessional circle as shown above. The obliquity oscillates between $22^\circ$ and $24^\circ$ once in 41,000 years. Currently the obliquity is decreasing by $47'' |
- | === - Precession, nutation | + | The actual reasons behind these motions lies in the physics of a spinning top. When you release a top, you exert a torque on the axis of the top and, hence, the axis rotates and oscillates. The details can be found in this [[uv: |
- | {{: | + | |
- | Celestial equator moves westward toward ecliptic at a rate of $5029.097$ arcsec | + | === - Barycentric coordinates === |
+ | The equatorial system is highly **non-inertial**, | ||
- | Around 4500 years ago, Thuban was the pole star. | + | In order create a more **inertial** frame of reference, IAU recommended [[uv: |
- | After 12,000 years, Vega will be the pole star. | + | ==== - Measuring RA-DEC ==== |
+ | RA and DEC are traditionally measured using **transit telescopes** (or **meridian circles**). A transit telescope always points toward an observer' | ||
- | Unlike the **lunisolar** precession, **planetary** precession causes the obliquity to decrease by $47$ arcsec per century. | + | {{: |
- | {{https:// | ||
- | |||
- | International Celestial Reference System where the barycenter is the origin. | ||
- | |||
- | Equator defines the fundamental plane, but the poles and axis are determined by distant quasars creating an **inertial reference frame**. | ||
- | |||
- | ==== - Other Systems ==== | ||
- | North ecliptic pole, NEP: RA 18 hours, Dec = $90^\circ-\epsilon$ where $\epsilon$ is the **obliquity of the ecliptic**. | ||
- | |||
- | North Galactic pole, NGP: $\alpha = 12:49:00$, $\delta=+27.4^\circ$ (equator and equinox of 1950) | ||
===== - Distance measures ===== | ===== - Distance measures ===== | ||
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where $\Delta t$ is the time it takes for a radio signal to come back to earth after getting reflected from Venus. | where $\Delta t$ is the time it takes for a radio signal to come back to earth after getting reflected from Venus. | ||
- | ==== - Stellar parallax | + | ==== - Distance ladder |
- | {{:courses:ast201: | + | {{:uv:distance-ladder.webp? |
+ | ===== - Time ===== | ||
+ | TAI: International Atomic Time defines 1 SI second as 9, | ||
- | {{ : | + | A **astronomical day** = 86,400 SI seconds. But historically we have used the sun, not atoms, for measuring time. |
- | The tangent of the parallactic angle | + | {{: |
- | $$ \tan p = \frac{a}{r} $$ | + | This figure shows an Earth-sized clock from god' |
- | where $r$ is the distance to the object and $a$ is in au. For $p\ll 1$ we can approximate $\tan p = \sin p = p$ and | + | Local mean solar time = HA of the mean Sun + 12 hrs. |
- | $$ p = \frac{a}{r}. $$ | + | {{: |
- | If $a$ is in au and $p$ in arcsec, then $r$ is in parsec. | + | Equation of time = local apparent solar time - local mean solar time. It takes on values up to $\pm 15$ minutes |
- | 1 parsec | + | Universal time, UT = mean solar time at Greenwich. |
- | {{: | + | But even UT is not precise enough because Earth' |
- | For nearby star, measurements | + | IERS maintains UTC: Coordinated Universal Time (UTC). UTC is close to UT, but it uses SI seconds instead |
- | HIPPARCOS has parallax uncertainties of 0.97 mas for around 118k stars brighter than $m_V=8.0$. | + | Our legal time follows UTC but finds |
- | Explore Gaia: https://www.esa.int/ | + | Zone time = UTC + longitude correction for the zone. |
- | ===== - Time ===== | + | The zones are usually $15^\circ$ wide in longitude; as the earth rotates that much in 1 hour. Computer networks synchronize clocks using standard protocols like ITS and ACTS. |
- | TAI: International Atomic Time: | + | |
- | 1 s = 9, | + | Sidereal time = HA of the mean March equinox |
- | {{: | + | which follows the UT. Astronomers count days continuously from a reference day as |
- | Local apparent solar time = HA of the Sun + 12 hrs. | + | Julian date (JD) = number |
- | Local mean solar time = HA of the mean Sun + 12 hrs. | + | In many cases, JD is given instead |
- | + | ||
- | Equation of time = local apparent solar time 2 local mean solar time. | + | |
- | + | ||
- | {{: | + | |
- | Universal tine, UT = mean solar time at Greenwich. | + | J2000.0 = Julian epoch 2000.0 = 2000 Jan 1.5 UT = JD 2451545.0. |
- | + | ||
- | UTC uses SI seconds. | + | |
===== - Motion ===== | ===== - Motion ===== | ||
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Measure the ICRS coordinate of a star in 10-year intervals. If the position changes, we know that the star actually moved because ICRS is not affected by parallax or precession. | Measure the ICRS coordinate of a star in 10-year intervals. If the position changes, we know that the star actually moved because ICRS is not affected by parallax or precession. | ||
==== - Radial velocity ==== | ==== - Radial velocity ==== | ||
+ | Christian Doppler gave a lecture on 25 May 1842 at the Royal Bohemian Scientific Society in Prague, Czechia. | ||
+ | |||
+ | For small **redshifts** $z\ll 1$ | ||
+ | |||
+ | $$ \frac{\lambda-\lambda_0}{\lambda_0} = \frac{\Delta \lambda}{\lambda_0} = \frac{v_R}{c} = z $$ | ||
+ | |||
+ | {{: | ||
+ | |||
+ | Resolving power of a spectrograph | ||
+ | |||
+ | $$ R = \frac{\lambda}{\delta\lambda} $$ | ||
+ | |||
+ | For large redshifts $z \gg 1$ | ||
+ | |||
+ | $$ z = \frac{\sqrt{1-\beta^2}}{1-\beta}-1 $$ | ||
+ | |||
+ | where | ||
+ | |||
+ | $$ \beta = \frac{v_R}{c} = \frac{(z+1)^2-1}{(z+1)^2+1} $$ | ||
+ | |||
courses/ast201/4.1698820364.txt.gz · Last modified: 2023/11/01 00:32 by asad