OWAO 2024, Практически тур — Задача 3. Ephemeric Quest

2024 ⋄ Practical Round ⋄ Problems · 20 т.

Указания
  1. The practical round is 5 hours long and accounts for 30 % of the total grade.

  2. The maximum score for each problem is 20 points. The round total is 60 points.

  3. Paper and electronic versions of problems are identical. The necessary files can be downloaded from the testing system.

  4. Please present your solution as an electronic report, containing information about your work, plots and tables, intermediate and final results, and conclusions.

  5. Please include your participant code (string like AA-1) at the beginning of each report.

  6. Submit your report in PDF format. If necessary, also attach working files (images, source code, etc.). ZIP format archives are accepted. The maximum file upload size is 10 MB.

  7. During the practical round, you can use:

  • browser, e. g. Google Chrome/Chromium,
  • text editor, e. g. Microsoft Word/LibreOffice Writer/Google Docs,
  • spreadsheet editor, e. g. Microsoft Excel/LibreOffice Calc/Google Sheets.

You may also use:

  • development tools, e. g. Python & Jupyter Notebook,
  • graphic editors, e. g. Paint/GIMP,
  • other applications for data processing, analysis, report generation, including online applications (Google Colab, Desmos, etc.).
  1. This is an individual competition. You must not use collaborative tools and functions.

  2. You may find and use documentation for the software and libraries used but not reference literature on astronomy, physics and mathematics.

  3. Please remember that the jury may not understand your language. It is expected that solutions are written in plain English. Use mathematical expressions, numbers and images.

  4. Some problems are quite difficult. Remember that partial solutions are also scored.

  5. A list of constants is given on page 8.

Go to https://my.sirius.online/, log in with your email and password, and select the Practical round. The countdown will begin after you click the Start button.

Good luck!

Условие

The file ephem.dat contains ephemerides of some small body of the Solar system. The first and second columns of the file contain the date and universal time of the observation, followed by the right ascension (in hours, minutes and seconds) and declination (in degrees, minutes and seconds) for the observer on the Earth (geocentric location):

DateTimeRight ascensionDeclination
2023-Mar-1800:00:0023h 59m 03.88s23^{\mathrm{h}}\,59^{\mathrm{m}}\,03.88^{\mathrm{s}}0∘ 44′ 46.9′′0^{\circ}\,44'\,46.9''
2023-Mar-1900:00:000h 0m 41.94s0^{\mathrm{h}}\,0^{\mathrm{m}}\,41.94^{\mathrm{s}}0∘ 55′ 34.0′′0^{\circ}\,55'\,34.0''
…………

The absolute magnitude of the object is H=18.51mH = 18.51^{\mathrm{m}}. The orbit of the object is circular, the inclination is small.

Please include your participant code at the beginning of your report.

a) Determine whether the object’s orbit lies inside or outside the Earth’s orbit.

b) Estimate the radius of the object’s orbit.

c) Estimate the minimal time interval between two consecutive greatest elongations or consecutive quadratures.

d) Determine the difference between the maximal and minimal apparent magnitudes of the object for an observer on the Earth during one synodic period.

e) Plot the dependence of the apparent magnitude of the object on time for an observer on the Earth during one synodic period.

Hint: for the Solar system objects, the absolute magnitude, commonly called HH, is defined as the apparent magnitude that the object would have if it were one astronomical unit (1.00 au) from both the Sun and the observer, and in conditions of ideal solar opposition (the apparent phase is 1.00).

Отговори

Решение

Константи

Universal

Speed of lightc=3.00⋅108 m/sc = 3.00\cdot 10^{8}\ \mathrm{m/s}
Planck constanth=6.63⋅10−34 J⋅sh = 6.63\cdot 10^{-34}\ \mathrm{J\cdot s}
Boltzmann constantkB=1.38⋅10−23 J/Kk_B = 1.38\cdot 10^{-23}\ \mathrm{J/K}
Gas constantR=8.314 J/(mol⋅K)\mathfrak{R} = 8.314\ \mathrm{J/(mol\cdot K)}
Proton massmp=1.673⋅10−27 kgm_p = 1.673\cdot 10^{-27}\ \mathrm{kg}

Astronomical

Astronomical unit1 au=149.6⋅106 km1\ \mathrm{au} = 149.6\cdot 10^{6}\ \mathrm{km}
Parsec1 pc=206 265 au1\ \mathrm{pc} = 206\,265\ \mathrm{au}
Hubble constantH0=70 (km/s)/MpcH_0 = 70\ \mathrm{(km/s)/Mpc}

Sun

RadiusR⊙=6.96⋅105 kmR_{\odot} = 6.96\cdot 10^{5}\ \mathrm{km}
MassM⊙=1.99⋅1030 kg\mathfrak{M}_{\odot} = 1.99\cdot 10^{30}\ \mathrm{kg}
Absolute magnitudeM⊙=4.74mM_{\odot} = 4.74^{\mathrm{m}} (bol.)
Effective temperatureT⊙=5.8⋅103 KT_{\odot} = 5.8\cdot 10^{3}\ \mathrm{K}
LuminosityL⊙=3.828⋅1026 WL_{\odot} = 3.828\cdot 10^{26}\ \mathrm{W}

Earth

RadiusR⊕=6371 kmR_{\oplus} = 6371\ \mathrm{km}
Sidereal dayτ⊕=23h 56m 04s\tau_{\oplus} = 23^{\mathrm{h}}\,56^{\mathrm{m}}\,04^{\mathrm{s}}
Obliquity of eclipticε⊕=23.437∘\varepsilon_{\oplus} = 23.437^{\circ}
Surface gravityg=9.81 m/s2g = 9.81\ \mathrm{m/s^2}
Orbital periodT⊕=365.26dT_{\oplus} = 365.26^{\mathrm{d}}
Orbital eccentricitye⊕=0.0167e_{\oplus} = 0.0167
x⊕=283.3∘x_{\oplus} = 283.3^{\circ}

Mars

RadiusRM=3390 kmR_M = 3390\ \mathrm{km}
Sidereal dayτM=24h 37m 23s\tau_M = 24^{\mathrm{h}}\,37^{\mathrm{m}}\,23^{\mathrm{s}}
Obliquity (axial tilt)εM=25.192∘\varepsilon_M = 25.192^{\circ}
Orbital semi-major axisaM=1.52 aua_M = 1.52\ \mathrm{au}
Orbital periodTM=1.88 yrT_M = 1.88\ \mathrm{yr}
Orbital eccentricityeM=0.0934e_M = 0.0934
xM=251∘x_M = 251^{\circ}

Оригинал в Архива: OWAO-2024-prob-P.pdf · официални решения: OWAO-2024-sol-P.pdf