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### Venus transit-a1-earth-sun-distance-final

1. 1.  EDUCATIONAL ACTIVITY 1.Calculating the Earth-Sun distance from images of the transit of Venus. Mr. Miguel Ángel Pío Jiménez. Astronomer Instituto de Astrofísica de Canarias, Tenerife. Dr. Miquel Serra-Ricart. Astronomer Instituto de Astrofísica de Canarias, Tenerife. Mr. Juan Carlos Casado. Astrophotographer tierrayestrellas.com, Barcelona. Dr. Lorraine Hanlon. Astronomer University College Dublin, Irland. Dr. Luciano Nicastro. Astronomer Istituto Nazionale di Astrofisica, IASF Bologna. 1 – Objectives of the activity. Through this activity we will learn to calculate the Earth-Sun distance (AstronomicalUnit) from digital images using the method of the solar parallax during the transit of Venus. The objectives are to: - Apply a methodology for the calculation of a physical parameter (Earth-Sun distance). - Apply knowledge of mathematics (algebra and trigonometry) and basic physics (kinematics) to derive this result. - Understand and apply basic techniques of image analysis (angular scale, distance measurement, etc.). - Work cooperatively as a team, valuing individual contributions and expressing democratic attitudes. 2 – Instrumentation. The activity will be based on digital images obtained during the transit of Venus in June2012 (see sky-live.tv). Please refer to the Glossary delivered with this document for a quickreference to terms used, abbreviations and physical units. 3 – Phenomenon. 3.1. Occultation and Transits. An occultation is the result of an alignment of one celestial body by another celestialbody as seen from Earth. A transit is a partial blackout phenomenon in which closer body desnot completely obscure the more distance body and the passage or transit of the closer oneprojected onto the surface of the background one is observed (Figure 2). From our planet we can only see the transits for the inner planets, Mercury and Venus,over the solar disk. Mercury moves in a plane that is 7 degrees tilted with respect to Earth’sorbit, so that most of the time Mercury goes “above” or “below” the solar disk, without causingtransits. Mercury tends to transit on average 13 times per century in intervals of 3, 7, 10 and 13years. The last transit of Mercury occurred on November 8, 2006. Venus  transit   1
2. 2.   3.2. The Transit of Venus. Venus, being closer to the Sun than Earth, also produces transists that are observable to us.Venuss orbital plane is inclined by 3.4° to Earth’s. Otherwise, there would be only a transit ofVenus every 584 days (the time it takes Venus to return to the same position with respect to theSun as seen from Earth). Each year Earth passes through the line of nodes (see Figure 1) of Venus’s orbit aroundJune 6-7 and December 9-10. If these dates coincide with inferior conjunction, i.e., when Venuslies between the Sun and the Earth, then there will be a transit. Figure 1: Illustration of the line of nodes of Venus orbit, when it intersects Earths orbit.   Transits of Venus are an extraordinarily rare phenomenon, since on average there areonly two per century. These two transits are separated by 8 years and the interval between pairsof transits alternates between 105,5 and 121,5 years. Sometimes, as it happened in 1388, one ofthe transits of the pair may not occur because it does not coincide with the passage by the node.The last pair of transits of Venus occurred on December 9, 1874 and December 6, 1882. The last transit visible from Europe took place on June 8, 2004 (Figure 2) and the nextone will be on June 6, 2012. Venus  transit   2
3. 3.   Figure 2: Venus’s Transit on June 8, 2004 showing the path of Venus across the solar disk at intervals of 45 minutes. Credits: Juan Carlos Casado © starryearth.com. From a visual point of view, the phenomenon of the transit of Venus is similar toMercury’s: Venus is visible as a black circle moving slowly over the brilliant solar disk. Thetransit of Venus lasts a maximum of 8 hours. During the transit, Venus has a very smallapparent diameter. However, it is clearly visible with the naked eye, properly protected, toobserve the Sun safely. A phenomenon called the “Black Drop” effect can also be observed atthe edges of the solar disk. The Black Drop effect. Just after the internal contact between the disks of the Sun andVenus, the disk of the planet seems to remain attached to the rim of the solar disk for a coupleof seconds, becoming deformed and assuming the shape of a black drop. This phenomenon isrepeated right before the last internal contact (Figure 3). The black drop effect prevents theaccurate measurement of the time of contact between the disk of the planet and the disk of theSun1. This was the main cause of the inaccuracy in the observations used to calculate thedistance between Sun and Earth. This effect was first attributed to Venus’ atmosphere. Howeverusing images of the transit of Mercury by the TRACE satellite (Transition Region and CoronalExplorer, NASA, USA) it was found2 that the main causes of the black drop effect are imageblurring (due to atmospheric seeing and telescope diffraction) and solar limb darkening. Thisimplies that the development of the black drop effect as seen by an observer on Earth dependsmainly on the atmospheric conditions and the quality of instrument used (e.g. size and optics oftelescope).                                                                                                                1 See a method to increase precision in contacts timing: http://www.transitofvenus.nl/blackdrop.html2 See the scientific paper: http://nicmosis.as.arizona.edu:8000/POSTERS/TOM1999.jpg   Venus  transit   3
4. 4.   Figure 3: Evolution of the black drop phenomenon during the ingress of Venus on the solar disk. Credits: Juan Carlos Casado © starryearth.com. The "Venus Aureole" effect. During the transits of Venus, a bright arc, about 0.1seconds of arc thick, has often been reported. It is seen around the circumference of Venus’ disk,which is partially outside the solar limb. It was the Russian scientist Mikhail Lomonosov whofirst described this effect when he observed the transit of Venus in 1761. Just after interiorcontact at egress, this aureole effect starts with the appearance of a bright spot of light near oneof the poles of Venus. Generally, this spot gradually grows into a thin arc as Venus movesfurther off the Sun (see Figure 4). At ingress, the phases occur in reverse order. The brightnessof the aureole is close to that of the solar photosphere, making it visible through a solar filter. Itcan only be seen under good observing conditions, using an excellent telescope. Figure 4: Venus Aureole effect detected in the 2004 Venus transit using the 1m Swedish Solar Telescope located on Roque de Los   Muchachos Observatory (La Palma , Instituto de Astrofísica de Canarias). Credit: D. Kiselman, et al. (Inst. for Solar Physics), Royal Swedish Academy of Sciences. The Aureole effect is caused by refraction of the Sun light in the dense upper atmosphereof Venus. Venus atmospheric conditions will determine the appearance of the aureole. If therefraction index of the atmosphere is small, the aureole already breaks into bright spots whenthe disk of Venus is just off the solar disk. But if the refraction index of the atmosphere is high,the aureole will extend all around the planet’s limb as a complete arc (see Figure 4). 3.3. Previous transits. 17th Century. The first recorded transit of Venus was on December 4, 1639. Horrocks, a Venus  transit   4
6. 6.  made worldwide, creating an international educational network to determine the astronomicalunit as a global experiment and a noteworthy event. 3.4. The Transit of Venus in 2012. The transit of June 5th − 6th, 2012 will be fully visible from the north of the Nordiccountries, the Far East, eastern Russia, Mongolia, eastern China, Japan, Philippines, Papua NewGuinea, central and eastern Australia, New Zealand, West Pacific Ocean, Alaska, northernCanada and nearly all of Greenland. From Spain it is only visible the end of the phenomenon atsunrise in the eastern region of the Iberian Peninsula and Balearic Islands (Figure 6). After thistransit, we must wait until the years 2117 and 2125 to see the next two transits of Venus, this FIGURE 1time in December. Global Visibility of the Transit of Venus of 2012 June 05/06 Region X* Greatest Transit at Zenith Tra t et nse Tra uns nsit t Su nsit at S Beg sa End ins IV I IV I ins End Transit No Entire sa Transit Beg III II III II at S Transit t Su in Progress nsit Transit in Progress nsit unr at Sunset Visible Tra nris Visible at Sunrise Tra ise e (June 05) (June 06) Region Y* F. Espenak, NASAs GSFC eclipse.gsfc.nasa.gov/OH/transit12.html * Region X - Beginning and end of Transit are visible, but the Sun sets for a short period around maximum transit. * Region Y - Beginning and end of Transit are NOT visible, but the Sun rises for a short period around maximum transit. Figure 6: World visibility of the 2012 transit of Venus. Credits: F. Espenak, (NASA / GSFC). 4 – Methodology 4.1. Methods to calculate the solar parallax during a transit of Venus. There are three main methods to calculate the solar parallax by combining observationsfrom two separate locations during the transit of Venus. A fundamental principle to consider is that the more distant in latitude the two observersare, the more accurate the measurement will be (e.g., one observer in the northern hemisphereand the other in the southern hemisphere). This is the method we will use, considering thelocations of our observations. I. Halleys method. Halley’s method in of observing and comparing the total duration of the transit. The exacttimes of the internal or external contacts of Venus and the solar disk must be calculated. Theobservations should be carried out from two places on Earth where the entire transit can beobserved. However problems can arise because of bad weather that can prevent the observation. Venus  transit   6
7. 7.   Figure 7: A diagram of the meaning of “Interior Contact” and “Exterior Contact”. II. Delisle’s method. In this method, the time of occurrence of the same contact event between the disk ofVenus and the solar disk is measured by geographically distributed observes. External contactsare often difficult to determine so the inner contacts are the best choice. The advantage over theHalley method is that it relies on only one contact being visible. III. Direct measurement of the parallax of Venus through images. Unlike the previous two methods, which rely on timing, in this method, simultaneousimages from two different geographical locations must be taken. The observable that ismeasured is the distance between the centers of Venus’s shadow over the Suns disk as seenfrom the two locations. A full description of this method is given in Appendix I. Figure 8: Simultaneous observation of the transit of Venus in front of the disk of the Sun from two different locations M1 and M2 at the same instant of time. We assume the geometry of the situation as shown in Figure 8. Point O is the centre ofthe Earth, C the centre of the Sun and V1 and V2 the observed centers of the projection of Venusseen from M1 and M2, respectively. The angles D1 and D2 are the angular separations betweenthe centers of Venus and the Sun seen from M1 and M2, respectively, i.e., the angles of parallaxCM1V1 and CM2V2. Similarly, we define the angles πs and πv as the angular separations between Venus  transit   7
8. 8.  M1 and M2 views from the Sun and from Venus, respectively, i.e., the angles M1CM2 andM1VM2. By definition we have, ! ! sin !! = ; sin !! = !! !!" where rT is the Sun-Earth distance distance, rVT is the Venus-Earth distance, and d is thedistance between M1 and M2 in a straight line. Appendix I describes how d may be determinated. We can make the following assumptions: • Since the distances between the objects are large, and the parallax is small, we can approximate the sin of the parallax to the parallax itself, i.e., sin πi ≈ πi. • The Earth, Sun and Venus are aligned, so that rVT = rT – rV (where rv is the Venus Sun distance). • The observation points M1 and M2 on Earth are along the same meridian, so that M1, M2, C and V are in the same plane (coplanar). • We also assume that these points are coplanar during all the transit; in fact this is not true since the Earth rotates and the geometry of the systems change during this rotation. We define Δπ = πV – πS. Since we have: ! ! !! =      and    π! =   !! !!   −   !!by substitution we can set, π! ·   r ! π!   =   !! − !! Since Δπ = πV – πS, we can substitute in for πv to get: !! !! !"   =   !! − 1   =   !! !! − !! !! − !! And so, !! ! !!   =  !" − 1   = !! !! Rearranging, we get the Earth-Sun distance, rT, at the time of observation to be: ! !! = !"  (! Equation [1] ! /!!  !  !)where Δπ is an observable quantity (distance between the centres of the shadow of Venus on thesolar surface in units of radians), d is determined from the locations (see Appendix II), and theratio rT / rV of the Sun-Earth and Earth-Venus distances can be obtained (see Appendix III). Ifwe express d in kilometres, then the Earth-Sun distance will be also in kilometres. The observable Δπ can be calculated in two ways described below, in sections 4.2 and 4.3(in practice in sections 5.2.1 and 5.2.2). Venus  transit   8
9. 9.   4.2. Method 1. Method of “The Shadows”. In this method, the transit in photographed from two different places at exactly the sameinstant, with the same type of instrument. The two images are then superimposed, and theangular separation, Δπ, between the centres of the shadow of Venus can be found. Details of theprocedure to be followed are found in paragraph 5.2.1. 4.3. Method 2. Method of "The Strings". In this case we will consider the whole trajectory of the shadow created by Venus on thesurface of the Sun (see Figure 2), created by Venus calling the line connecting the centrepositions of the shadow of Venus, string M1 or string M2, depending on the observing point onthe Earth to which it refers. Given that the Earth-Sun distance changes only slightly over the course of transit, (thechange is only 7,500 km compared to the average Earth-Sun distance of 150 million km) we canassume that the two strings are parallel and now the observable to be measured is not thedistance between the shadows of Venus but the distance between the two strings that are formedon the surface of the Sun during the transit (see Figure 9). Figure 9: A representation of the two “strings” on the surface of the Sun, A1A 2 and B1B2 as seen by observers at locations M1 and M2 on Earth. Using Pythagora’s theorem, we can write the following expressions: ! ! !! !! ! ! ! !! !! ! !! ! =   ! + ! !! ! =   ! + ! So we can express AB as: ! ! ! ! ! ! ! ! ! !! !! ! !! !! !! =! !−!! = + −   + 2 2 2 2 So measuring the length of the strings A1A2, B1B2, along with the diameter of the Sun(D), we can then obtain the parallax Δπ from, Venus  transit   9
10. 10.   1 Δπ = ! ! − !! !! ! −   ! ! − !! !! ! 2 5 – Calculations for the Transit of Venus, on 5/6 June 2012. 5.1. Putting ourselves in position. In this section we address, specifically, the next transit of Venus, trying to get as close aspossible to the situation we will find when we meet in June at the computer, watching the transitand trying, with the images that will be taken, calculate the Earth-Sun distance. We begin with abrief description of the instrumentation to be used as well as the latitude and longitude of thelocations where we will take the pictures, and all other information necessary to succesfullycomplete the calculations. 5.1.1. Locations of the observations and instrumental description. We begin by describing the observatiing locations where the photos are going to be taken.As described above, to simplify the calculations as much as possible, we selected two places onEarths surface with similar longitude, values which are: Cairns (Australia): Latitude: −16º 55 24.237" Longitude: 145º 46 25.864" Sapporo (Japan): Latitude: 43º 3 43.545" Longitude: 141º 21 15.755" The images will take in real time with a VIXEN telescope (model VMC110L), which hasa focal ratio of f/9.4, meaning a focal length of 1035 mm for its aperture of 110 mm. Thisconfiguration ensures an acceptable size for the Sun’s image. A solar filter will be used for theobservations. The images will recorded with a Canon 5D 21-Mpixel camera attached to thetelescope. With this Telescope and this camera, the Sun’s image has a size in the plane of thecamera, and therefore also in the image of 1630 pixels. Considering that the angular size of the Sun in the sky is about 31.5 minutes of arc, thenthe scale, ε, of the sun in the image will be: 31.5   !"#\$%&  !"  !"#  (′) · 60 !"#\$%&!  !"  !"#  (") !"#\$%  (!) = = 1.16  "/!"#\$% 1630  !"#\$%& The telescope and camera will be mounted on an “Astrotrack” mount, which is verystable and easy to assemble and tracks the Sun’s movement across the sky. Images will be recorded every 5 minutes throughout the duration of the event, the orderof 5 hours. After some simple processing, they will be put in real time on a ftp server, to permiteasy and free access thereto, to acquire and make the practice. Each of the images, when saved,will contain the time (in UT) when the image was taken in the filename. Venus  transit   10
11. 11.     Figure 10: A photograph of the Instruments. Credits: M. A. Pío (IAC). 5.2. What we need to do in practice. In Sections 5.2.1 and 5.2.2 we explain the practicalities of determining Δπ using the twomethods described earlier. If time permits, we suggest using both methods and comparing theresults obtained. 5.2.1. Method 1. Method of “The Shadows”. We start with two images taken at the same instant of universal time (or as close aspossible), one at each location. We have to determine the distance between the shadows ofVenus. To calculate the distance Δπ we should align the two images (rotation and translation asboth have the same scale) and take the measurement of the distance between the shadows ofVenus using an imaging software package. However, to simplify the process and remove theneed for the images to be aligned, we have made some mathematical transformations todetermine the distance using, (i) the Cartesian (x, y) coordinates of the shadow of Venus; (ii) aspot on the solar surface and (iii) the centres of the Sun in each image. Figure 11 shows the Venus  transit   11
12. 12.  observations (using astronomical software) during the transit (time 0:45 UT of the day June 6,2012) from the two observation locations, in Cairns (Australia) and Sapporo (Japan). Note thatthe distance which separates the two shadows (Δπ) will be very small, being of the order of 10pixels maximum.Figure 11: A real image of the Sun made with the instrumentation that will be used for the transit, with a fictionalrepresentation of the phenomenon at 00:45 UT of June 6, 2012. Following the calculations in Appendix IV, the observable Δπ is determined from theexpression: ! Δ! = Δ!! ! + Δ!! !where the components Δπx and Δπy can be expressed as: Δ!! = !! − !!! cos ! + !! − !!! sin ! − !! + !!! Δ!! = − !! − !!! sin ! + !! − !!! cos ! − !! + !!"where (x1, y1) and (x2, y2) are the coordinates of the shadow of Venus in the images fromSapporo and Cairns, respectively, while (xc1,yc1), (xc2, yc2) are the coordinates of the centre ofthe Sun from Sapporo and Cairns, respectively, all referred to the coordinate system S. In our case, for the day of June 6, 2012 and observing from Cairns in Australia, andSapporo in Japan, the angle θ is (see calculations in Appendix IV): θ = 108º 4 17.92" So: ! Δ! = Δ!! ! + Δ!! ! = 8.4  !"#\$%& Appendix I presents a very precise method to determine the value of the distance dbetween the two observers on Earth. In our case, the value of d is: Venus  transit   12
13. 13.   d = 6662.9 km Recalling Equation [1], we also require the ratio of the Earth-Sun and the Venus-Sundistance (rT / rV) at the time of the observation. The term of Δπ in this method, must be in seconds of arc, so you have to make use of thescale value to be determined at the moment. For the case of the image that we produce using theastronomical software, the value of Δπ is 8.4 pixels, and whereas the diameter of the sun inpixels is 715 pixels, which gives a scale of: 31.5   !"#\$%&  !"  !"#   ′ · 60 !"#\$%&!  !"  !"#  (") !"#\$%  (!) = = 2.643"/!"#\$% 715  !"#\$%& Note that this is only in this case, using the sizes of the Figure 11, and in the moment ofthe Transit, the scale that we need to use, is the one that we put in Section 5.1.1. So we use rT / rV = 1,39759 at 0:45 UT on June 6, 2012 (a value obtained fromephemerides to that date), and substituting into Equation [1]. 6662.9   !"!! = = !"#. ! · !"!  !" !"#\$%#&( ! !"# 8.4   !"#\$%& · ε · (1.39759 −  1) !"#\$%& 648000 !"#\$%#&( can determine the value of rT, the distance from Earth to the Sun. Rcall that the value ofΔπ must be expressed in radians, hence the term π / 648000, which makes the change of units(from seconds of arc to radians). 5.2.2. Method 2. Calculation of the Earth-Sun distance using the string method. This method is easier than the previous one, since we need only to determine the lengthsof lines or strings that create the path of the shadow on the surface the Sun. For this reason, wewill not have the problem we had in the previous method in which we had to have a very tightlysynchronised observations between the two places on Earth, when taking the images, to ensurethat both have been taken at the same instant. However, the string method can only be appliedwhen the transit is completed. On the other hand, an advantage is that if the weather turns badduring the transit or there are technical problems which result in some missing images, we onlyhave to extrapolate to the rest of the trayectory. We must bear in mind that the images of each spot must be aligned, throughout thetransit, since due to the rotation of the Earth essentially, the Suns image will rotate during thetime of the transit, so that the trajectory of the shadow instead of being rectilinear, is curved. Be aware that the distance between the two strings will be very small, so the length ofboth strings might be very similar. We will need, as explained above, the value of the solar diameter (D), and the length ofthe lines M1 and M2, all measured in the same units. Figure 12 shows a representation of what might be seen using this method and anastronomical software. Venus  transit   13
14. 14.   Figure 12: An image made with astronomical software, with a simulated representation of the strings. The lengths of the lines M1 and M2, based on this image, are join A1 to A2 and B1 B2,respectively (see Figure 9), and can be measured, both in mm or pixels, depending on whetherthe measurement is made with a ruler after printing the image, or using software that allows usto represent and manipulate images. Proprietary software, such as Photoshop or Corel Draw, oreven Windows Paint, or free software like Gimp can be used for this task. Basically, anysoftware that allow us to calculate the sizes of objects within an image can be used. Note: If you want to measure the longitude of the strings in mm, you must be coherentwith the units. This means you need to recalculate the scale factor (see page 17) using thediameter of the Sun in mm. The scale, ε, will then be [arcsec/mm]. For the sample image, the value of Suns diameter D, in pixels, is 711, and the string M1(B1B2) measures 565 pixels, and the string M2 (A1A2) measures 578 pixels. We now need tocalculate the ratio AB, where AB is, according to Figure 9, the distance between the twostrings, a distance which is directly related to the value of Δπ. Thus, the expression that we useis: 1 Δ! = !! ! ! = ! ! − (!! !! )! −   ! ! − !! !! ! = 8.79  !"#\$%& 2 Finally, substituting into Equation [1]: 6662.9   !" !! = = !"#. ! · !"!  !" !"#\$%# ! !"# 8,79   !"#\$%& · ε · (1.397589 −  1) !"#\$%& 648000 !"#\$%# where, again, the value of rT is the distance Earth-Sun distance,   d is the distance betweenobservers, determined according to Appendix II, ε is the scale value described, and the ratiorT/rV is the average value for the transit. One factor to take into account and not previously discussed is that the value of the radiusvector connecting the Earth to the Sun, and its counterpart linking Venus with the Sun, bothvary with time because the orbits of both Earth and Venus are elliptical. Therefore, in Method 1,which considers a fixed point in time (0:45 UT in the example), the ratio rT / rV has to be theinstantaneous value at that time, but in the case of Method 2, the value of the ratio rT / rV to be Venus  transit   14
15. 15.  used is the average value over whole transit. However, we can see that both values differ onlyslightly, because in such a short period of time (just over 5 hours of the transit), the variation inthe Earth-Sun distance is negligible (see Appendix III) . 6 – Useful Internet Resources.• Online predictions of the Transit of 2012: http://www.transitofvenus.nl/details.html• General Information an data over the transit: http://www.transitofvenus.org• Safe methods for solar observation: http://www.transitofvenus.org/june2012/eye-safety• Data and Predictions: http://eclipse.gsfc.nasa.gov/OH/transit12.html• The live transmission of the transit through the Internet: http://www.sky-live.tv• Scientific expeditions of Shelios group to observe astronomical phenomena:   http://www.shelios.com  • Description of the Kepler’s laws.   http://csep10.phys.utk.edu/astr161/lect/history/kepler.html  • Description of the calculation referred to the solar parallax with examples:   http://serviastro.am.ub.es/Twiki/bin/view/ServiAstro/CalculTerrasolapartirDeVenus and http://www.imcce.fr/vt2004/en/fiches/fiche_n05_08_eng.html Venus  transit   15
16. 16.   APPENDIX I. Calculations of Method 1 in depth. The determination of the Earth-Sun distance is based on the parallax effect (as seenabove) whereby, from two different locations, Venus is projected onto different locations on thesolar disk. Therefore it must combine observations from different places on Earth. The fartherapart are the two places of observation the more relevant is this effect of perspective and, thus,we will be able to obtain a more accurate distance measurement. The observations must be complemented by Kepler’s laws which describe the orbits ofthe planets around the Sun. These laws were discovered by Johannes Kepler (1571−1630) usingmany observations of planetary motion. The law of universal gravitation, formulated by IsaacNewton (1642−1727), applied to the case of two moving bodies around a common centre ofmass, explains the three empirical Kepler’s laws. From two different locations M1 and M2 (see Figure 13 and Figure 8) and at the sametime t, Venus is projected in two different positions V1 and V2 on the solar disk due to theparallax.Figure 13: Observation of the transit of Venus in front of the solar disk from two different locations M1 and M2 at thesame instant of time.   Point O is the centre of the Earth, C the centre of the Sun and V1 and V2 the observedcentres of the projection of Venus as seen from M1 and M2, respectively. The angles D1 and D2are the angular separations between the centres of Venus and the Sun seen from M1 and M2,respectively, i.e., the angles of parallax CM1V1 and CM2V2. Similarly, we can define the anglesas πV πS and angular separations between M1 and M2 seen from the Sun and from Venus,respectively, i.e., the angles and M1VM2 M1CM2.   Since the four points M1, M2, C and V are not in the same plane (the most common casewill not have both sites M1 and M2 on the same meridian, or Earth-Venus-Sun perfectly aligned),the geometry of the problem is a bit complicated. In Figure 8 (and also in Figure 13) you can seehow the distance between the two centres of Venus Δπ = πV – πS is (hardly) the only observablequantity which allows to calculate the distance to the Sun. The practical realization of the measure of Δπ from the two images separately can bemade by measuring the position of the centre of Venus in each of them respect to a referencepoint on the solar disk (a solar spot, for example) and comparing the two measurements.Measured quantities are taken in units of length, for example in millimetres, and should beconverted to an angle that you can get by knowing the apparent diameter of the Sun. Venus  transit   16
17. 17.   Let (x1, y1) and (x2, y2) be the separations between the centre of the disk of Venus and thespot of reference, in mm, in the horizontal and vertical directions for each image. Theseparations in arcseconds are obtained by multiplying each of the quantities x1 and y1 by thefactor of scale (ε). !"#\$%  !"!"#\$%&  !"#\$%&%  (!"#\$%#) !"#\$%  (ℇ) = !"#  !"#\$%&%  (!!  !"  !"#\$%&) The distance between the centres of Venus in the two images will be: Δπ (arcsec) = [(x2 − x1)2 + (y2 − y1)2 ]1/2 · ε Figure 14: Positions of the projection of Venus over the Suns disk. Suppose rV and rT are the distances between the centre of the Sun and Venus and Earth,respectively, at time t of observation. Since the projection of the distance d between M1 and M2in the plane perpendicular to OC is small compared to the distances Earth-Sun and Earth-Venus,we can approximate: πS = d/rT πV = d/(rT − rV) and from here, we can obtain: πV = πS rT/(rT − rV) Δπ = πS (rT/(rT − rV) − 1) = πS rV/(rT − rV) so, πS = d/rT = Δπ (rT/rV − 1). The latter formula expresses that if we know the angular distance, Δπ, between the twocentres V1 and V2, and the ratio rT / rV between the distances Earth-Sun and Venus-Sun, theparallax πS can be obtained, and knowing the projected distance d between the two locations, wecan calculate the distance rT. (In all these expressions the values of πV, πS and Δπ are given in Venus  transit   17
18. 18.  radians. To convert to arcseconds and make them compatible with equations, one need only tomultiply by 648000 and divide by the number π). Δπ is the observable quantity, d can be determined using the locations in the Earth (seeAppendix II) and, therefore, the only quantity needed to solve the problem is the ratio rT/rV, theEarth-Sun and Venus-Sun distances. Determination of the average distance. On other hand, we can also determine the average distance Earth-Sun (RT) and thecorresponding average parallax πo, which are related through Earths equatorial radius R by: πo ≈ R/RT,and to do that, it is necessary to make some additional considerations. The average distance Earth-Sun, RT, can also be defined as the radius that would have theorbit of the Earth if it were a circle with the center coincident with the center of the ellipse thatdefines the actual orbit. In this case the RT value matches the value of the semi-major axis of theorbit a (a=1,000014 RT). So we can express the value of the medium parallax as: ! ! ! !! ! ! ! !! !! = = ·   = !! ·   ⟹   !! = · · !! !! ! ! ! !! ! !! ! !where rT/a is the ratio between the Earth-Sun instant distance and the semi-major axis of Earth’sorbit. Based on the above expression πo ≈ R / RT, we can then derive the value of RT, which isthe average of the value of the Earth-Sun distance. Venus  transit   18
19. 19.   APPENDIX II. Determine the value of d. If you express the projection d of the distance between M1 and M2 in the plane normal tothe direction Earth-Sun in units of Earth’s equatorial radius and the Earth-Sun distance in unitsof the average distance, we have: πS = [(d/R) / (rT /RT)] (R/RT) ≈ [(d/R) / (rT /RT)] πo. The ratio rT / RT can be calculated from Keplers first law as: rT/RT = 1 − eT cos ET(t) and therefore we only need to calculate d/R (see Figure 8). Figure 15: Projection of the distance between M1 and M2 in the plane normal to the Earth-Sun direction. Making the vector product between the vectors M1M2 and OC, we obtain the value of sinθ, because: M1M2 × OC = |M1M2| rT sin θ. In Figure 15 you can observe that: d = |M1M2| cos (90 − θ) = |M1M2| sin θ and therefore, d = M1M2 × OC / rT. Now, we need to calculate M1M2 × OC. The OC vector can be expressed from the equatorial coordinates of the Sun (α,δ) at time tof observation as: x = rT cos δ cos α y = rT cos δ sin α z = rT sin δ. The position of each observer can be expressed as (see Figure 16): Venus  transit   19
20. 20.   x = R cos φ cos (λ+TG) y = R cos φ sin (λ+TG) z = R sin φ,where φ and λ are the geographical coordinates (latitude and longitude) of the observer and TGis the sideral time of each point of the Earth who has a longitude λ. In our case, on June 6th 2012,the value is TG (0h UT) = 16h 59m 12.495s. 360! !! = !! 0 + · ! →   !! = !! (0)   +  1.00273791  ! 23! 56! 4.1 ! M1M2 vector coordinates can be found easily as: X = x1 − x2 Y = y1 − y2 Z = z1 − z2 !! !! =  !! + !! + !! ! !! !! =   !! + !! + !!and the coordinates for the unitary vector c, which connect the center of Earth with the Solarcenter would be: x = cos δS cos αS y = cos δS sin αS z = sin δS So going back to the expression of d, it can be expressed as:! =   !! !! sin ! =   !! !!  ×  ! =   !" − !" ! + (!" − !")! + (!" − !")!       Figure 16: Positions of a star (e.g. the Sun) and an observer on Earth in equatorial coordinates. Venus  transit   20
21. 21.   APPENDIX III. Kepler’s Laws. The subject of planetary motion is inseparable from a name: Johannes Kepler. Keplersobsession with geometry and the supposed harmony of the universe allowed, after several failedattempts, to create the three laws that describe with great precision the movement of the planetsaround the Sun. Starting from a cosmological Copernican position, which at that time was morea philosophical belief than a scientific theory, and using the large amount of experimental dataobtained by Tycho Brahe, Kepler created this wonderful, though entirely empirical, set of laws. The first law states that the planets describe elliptical orbits around the Sun, whichoccupies one focus. With Kepler’s disappointment, the circle occupied a privileged place; thisafter multiple attempts to reconcile the observations with circular orbits. 1. – First Law: "The orbit that describes each planet is an ellipse with the Sun at one focus". Figure 17: Description of the elements of an objects orbit around the Sun. Elliptical paths have very small eccentricity, so that differ little from a circle. Forexample, Earths orbit eccentricity is e = 0.017, and given the Earth-Sun distance of about150,000,000 km, the distance from the Sun (focus) to the center of the ellipse is ae = 2,500,000km. The second law refers to the areas swept by the imaginary line connecting each planet tothe Sun, called the radius vector. Kepler found that planets move faster when they are closer tothe Sun, but the radius vector covers equal areas in equal times. (If the planet takes the sametime going from A to B in the figure, from C to D, the shaded areas are equal). 2. – Second Law: "Every planet moves so that the radius vector (line joining the center of the Sun to the planet) sweeps out equal areas in equal times". Venus  transit   21
22. 22.   Figure 18 : Graphical representation of Kepler’s 2nd law. The radius vector r, ie the distance between the planet and the Sun (S) is variable, it isminimum at perihelion and maximum at aphelion. As the areal velocity (swept area in unit time)is constant, the velocity of the planet in its orbit must be variable. Under this law, if areas CSDASB and are equal, the arc AB will be less than the CD, indicating that the planet moves slowerat aphelion. That is, its velocity is maximum at the minimum distance from the Sun andminimum to maximum distance. Finally, the third law relates the semi-major axis of the orbit, R, the planets orbital periodP, as follows: R3/P2 = constant. According to this law, the duration of the orbital path of a planetincreases with distance from the Sun and we know that the "year" (defined as the time taken bythe planet to return to the same point in its orbit) of Mercury has 88 days (terrestrial), Venus 224,the Earth 365 and it continues to increase as we move away from the Sun. These laws also allowto obtain the relative distances of objects in the solar system, if we know their movements. 3. – Third Law: "The square of the periods of revolution of two planets is proportional tothe cubes of their mean distances from the Sun". Figure 19 :Relationship between the periods and radii of the orbits around the Sun of two objects, which graphically describes Kepler’s 3rd law. Venus  transit   22
23. 23.   If R1 and R2 are the mean distances of two planets to the Sun, such as Mars and Earth,and P1 and P2 are the respective times of revolution around the Sun, according to this law it is: ! ! !! !! ! = ! !! !!where time is given in years and distance in astronomical units (AU = 150,000,000 km). Following the statement of the law made by Kepler, Newton proved that in the equationthe masses of the bodies should be present, and thus he obtained the following formula: ! ! !! (! + !! ) !! ! = ! !! (! + !! ) !!where M is the mass of the Sun (body located in the center of the orbit), equal to 330,000 timesthe mass of the Earth, and m1 and m2 are the masses of the considered bodies that move inelliptical orbits around it. This expression allows to calculate the mass of a planet or satellite, ifthe orbital period P and its average distance to the Sun are known. Overall for the planets of the solar system only the mass of Jupiter and Saturn are notnegligible with respect to the Sun. Because of this, in most cases (M + m) is considered equal to1 (solar mass) so that the expression becomes the one originally given by Kepler. For the first time a single geometric curve, without additions or components, and a singlerate law is sufficient to predict planetary positions. Also for the first time, the predictions are asaccurate as the observations. These empirical laws found their physical and mathematical support in Newton’suniversal gravitation theory, who established the physical principles that explain planetarymotions. The construction of this body of ideas, that begins with Copernicus and culminated inNewtons mechanics, is a prime example of what is considered a scientific procedure, which canbe described very briefly as follows: there is a fact, take measurements and draw up a data table,then try to find the laws that relate these data and, finally, carefully investigate before to decideto support or explain the law. On the other hand, new or more precise measurements can showthat a law or theory is wrong or approximate so that a new one is required. Einstein’s law ofgravitation is an example. Application in the present case. The orbits of Earth and Venus around the Sun are slightly elliptical and thus the ratio ofthe distances rT/rV is not constant over the time. To find this ratio at time t of observation isnecessary to refer to Keplers first law, which says that the Sun is one of the foci of the ellipseand, thus, the distance between the Sun and a planet rp (t) can be obtained as: rp(t) = Rp (1 − ep cos Ep(t)), Venus  transit   23
24. 24.   Figure 20: Section of ellipse showing eccentric (E) and true (θ) anomaly.where Rp is the semi-major axis of the orbit, ep is the eccentricity and Ep(t) the eccentricanomaly (angle measured from the centre of the ellipse, which is the angle between theprojection of the planet on the so called auxiliary circle, and the ellipse major axis, see Figure16) at time t. So, according to this rT/rV = [RT (1 − eT cos ET)] / [RV (1 − eV cos EV)] Keplers third law links the semi-major axes of the orbits with periods of revolution Pp: (RT / RV)3 = (PT / PV)2, so that: rT/rV = (PT / PV)2/3 (1 − eT cos ET) / (1 − eV cos EV) [2] So far we have determined πS and rT, which are the parallax and the Earth-Sun distance atthe instant t of observation. Venus  transit   24
25. 25.   APPENDIX IV. Calculation of the rotation / translation of theimages. As we discussed in paragraph 5.2.1, if we take an image of the Sun from a place onEarths surface at a given instant of time t, and at exactly the same time we take another picturefrom another location far enough from the first, these two images will be rotated by an angle θwhich depends directly on the separation of these two positions on the Earth. In addition, if thetelescope pointings are not exactly the same, a translation will also be present between the twoimages. We must remember that the images were taken with the same instrumentation and,therefore they have the same scale. Coordinate Systems of S and S. Suppose two coordinate systems. We call one S and is located in the center of the Sunand the other S which, for convenience, place in the lower left corner of the image (see Figures21 and 22). A really important thing is that S is the same for both images. Figure 21: Diagram of the graphical representation of used systems. The transformation equations for translation between the two systems are: xi1 = xi1 − xc1 ; xi2 = xi2 − xc2 yi1 = yi1 − yc1 ; yi2 = yi2 − yc2where (xc1, yc1), (xc2, yc2) are the coordinates of the center of the Sun as observed in Sapporo andCairns, respectively, in the coordinate system S. (xi1, yi1), (xi2, yi2) are the coordinates of a pointmeasured on the two images, S system, and (xi1, yi1), (xi2, yi2) are the correspondingcoordinates using the reference system S centered on the Sun. Venus  transit   25
26. 26.   Measurement of the angle θ. Once we have all the items referred to the coordinate system S centered on the Sun, wewill calculate the value of the angle θ by calculating the difference between the angles formedby the vector T2 relative to the Spot on the image of Cairns, and the same Spot on the image ofSapporo T1, through the expression (scalar product): T! ! · T! ! = T! ! ·  T! ! · cos  θ !′!! · ! ! !! + !′!! · ! ! !!   ⟹ cos ! = T! ! · T! ! = !′!! · ! ! !! + !′!! · ! ! !! ! !′! + !′! · ! !′! + !′! !! !! !! !! Δπ calculating the coordinate system S Finally we are going to calculate the distance value Δπ referred to the system S, whosezero is located in the lower left corner of the image.Figure 22 : Vector diagram for each point according to the systems S (centre of the Sun) and S (bottom left image). According to Figure 22, we can express the vector T1, T2, R1 and R2 in terms of vectors Scentred on the Sun, and the vector c from the origin of coordinates of S with S, as: !! = ! + !! !                                    !! = ! + !! ! On the other hand, the expression of Δπ we have above can also be expressed in terms ofthe coordinates, so that the total value is: Venus  transit   26
27. 27.   ! Δ! = Δ!! ! + Δ!! ! So: !! ! !! !! ! !! Δ!! = !! − !! = !! − !! + !!                          Δ!! = !! − !! = !! − !! + !!where (x2", y2") are the coordinates of the shadow of Venus in Cairns in the reference system Srotated by the angle θ, and using the transformation equations for rotation and translation tocoordinates on S we will have: !! ! Δ!! = !! − !! = !! − !!! cos ! + !! − !!! sin ! − !! + !!! !! ! Δ!! = !! − !! = − !! − !!! sin ! + !! − !!! cos ! − !! + !!!where (x1, y1) and (x2, y2) are the coordinates of the shadow of Venus in the images of Sapporoand Cairns, respectively, while (xc1, yc1), (xc2, yc2) are the coordinates of the centre of the Sun inSapporo and Cairns, respectively, all referred to the coordinate system S. Venus  transit   27
28. 28.   APPENDIX V. GLOSSARY. Arcminute (minute of arc) Is a unit of angular measurement equal to one sixtieth (1 ⁄ 60) of one degree or (π ⁄10,800) radians. Since one degree is defined as one three hundred and sixtieth (1 ⁄ 360) of arotation, one minute of arc is 1 ⁄ 21,600 of a rotation. Arcsecond (second of arc) An angular measurement equal to 1 / 60th of an arc minute or 1 / 3600th of a degree. It is 1⁄ 3,600 of a degree, or 1 ⁄ 1,296,000 of a circle, or (π ⁄ 648,000) radians. Astronomical Unit (AU) The astronomical unit is a unit of length used by astronomers, usually to describedistances within planetary systems such as our Solar system. One AU is equal to 149,597,871km, and corresponds to the average distance from the Earth to the Sun. Blurring It is said when an image is not clear and it seems not well focussed. This is due toatmospheric seeing and telescope diffraction. Center of mass The center of mass or barycenter of a body is a point in space where, for the purpose ofvarious calculations, the entire mass of a body may be assumed to be concentrated. Diffraction Diffraction is the ability of a wave to bend around corners. The diffraction of lightestablished its wave nature Eclipse It is the obscuration of a celestial body caused by the interposition of another bodybetween this body and the source of illumination. Ecliptic The ecliptic is the path that the sun appears to follow across the celestial sphere over thecourse of a year. Indeed, it is the plane defined by the Earths orbit around the Sun. Ephemeris An ephemeris is a table listing the spatial coordinates of celestial bodies and spacecraft asa function of time. Filter A filter is an optical device that blocks certain types of light and transmits others. Inastronomy filters are mostly used to study light from a source in one particular colour, i.e. in aparticular wavelength region, which can yield information on the chemistry of the object. Flux The flux is the measure of the amount of energy given off by an astronomical object overa fixed amount of time and area. Galilean moons The name given to Jupiters four largest moons, Io, Europa, Callisto & Ganymede. Venus  transit   28
29. 29.   Gravity Gravity is a mutual physical force of nature that causes two bodies to attract each other.The more massive an object, the stronger the gravitational force. Inferior conjunction A conjunction of an inferior planet that occurs when the planet is lined up directlybetween the Earth and the Sun. Inferior planet A planet that orbits between the Earth and the Sun. Mercury and Venus are the only twoinferior planets in our solar system. Latitude Latitude is the angular distance north or south from the equator of a celestial object,including the Earth. Limb The outer edge of the apparent disk of a celestial body. Longitude Longitude, on Earth, is a geographic coordinate that specifies the east-west position of apoint on the Earths surface. It is an angular measurement, usually expressed in degrees, minutesand seconds. Specifically, it is the angle between a plane containing the Prime Meridian and aplane containing the North Pole, South Pole and the location in question. If the direction oflongitude (east or west) is not specified, positive longitude values are east of the Prime Meridian,and negative values are west of the Prime Meridian. The closest celestial counterpart toterrestrial longitude is right ascension. Meridian The meridian is an imaginary north-south line in the sky that passes through theobservers zenith. Micron A micron or micrometre is one-millionth of a metre. Node One of the two points on the celestial sphere associated to the intersection of the plane ofthe orbit and a reference plane. The position of the node is one of the usual orbital elements. Nucleosynthesis Nucleosynthesis is the production of new elements via nuclear reactions. Nucleosynthesistakes place in stars. It also took place soon after the Big Bang. Occultation Occultation is an event that occurs when one celestial body conceals or obscures another.For example, a solar eclipse is an occultation of the Sun by the Moon. Opposition A planet is in opposition when the Earth is exactly between that planet and the sun. Orbit Venus  transit   29
30. 30.   The term orbit denotes the path an object follows around a more massive object orcommon center of mass. Parallax Parallax is the apparent change in position of two objects viewed from different locations.It is caused only by the motion of the Earth as it orbits the Sun. Parsec A parsec is a unit of distance commonly used in astronomy and cosmology, the parsec isequal to about 3.262 light years, or 3.09 × 1016 metres. It is the distance at which a star wouldhave a parallax of 1 arcsecond. Periastron The point of closest approach of two stars, as in a binary star orbit. Opposite of apastron. Perigee The perigee is the point in the orbit of the Moon or other satellite at which it is closest tothe Earth. Perihelion The perihelion is the point in the orbit of a planet or other body where it is closest to theSun. The Earth is at perihelion (the Earth is closest to the Sun) in January. Planet A planet is a celestial body orbiting a star or stellar remnant that is massive enough to berounded by its own gravity, is not massive enough to cause thermonuclear fusion and hence itdoes not shine on its own. Refraction Refraction is the change in direction of a wave due to a change in its speed. Resolution (spatial) The spatial resolution is the ability of an instrument mounted on a telescope todifferentiate between two objects in the sky which are separated by a small angular distance.The closer two objects can be while still allowing the instrument to see them as two distinctobjects, the higher the spatial resolution. Resolution (spectral or frequency) The spectral resolution is the ability of an instrument mounted on a telescope todifferentiate two light signals which differ in frequency by a small amount. The closer the twosignals are in frequency while still allowing the instrument to separate them as two distinctcomponents, the higher the spectral resolution. Revolution Revolution is the movement of one object around another. Seeing The term seeing in astronomy is used to describe the disturbing effect of turbulence in theEarths atmosphere on incoming starlight. Superior conjunction Venus  transit   30
31. 31.   A conjunction that occurs when a superior planet passes behind the Sun and is on theopposite side of the Sun from the Earth. Superior Planet A planet that exists outside the orbit of the Earth. All of the planets in our solar systemare superior except for Mercury and Venus. Transit Transit is when a smaller astronomical object passes in front of a larger one. During thistime, the smaller object seems to be crossing the disk of the larger one. Transit is also thepassage of a celestial body across an observers meridian. Universal time Universal time (abbreviated UT or UTC) is the same as Greenwich Mean Time(abbreviated GMT) i.e., the mean solar time on the Prime Meridian at Greenwich, England(longitude zero). Venus  transit   31