IOAA 2023, Отборен тур — Задача 3. Mars loop

Group Competition

Указания
  • For this round, the participants will be grouped by random selection into 5-person teams, each representing a named asteroid. Each participant in the group will be from a different country. The selection will take place near the beginning of the IOAA, so that the team members can get to know each other.
  • Please remember the name and number of your asteroid, as this will also be used to identify your place during the Planetarium and Observation rounds.
  • The group competition consists of several tasks, which you will receive in a sealed envelope. Each team works together at one table under the supervision of the guides to solve the tasks. You are not allowed to communicate with participants from other teams during the round.
  • Dedicated answer sheets are provided for writing your answers. Enter the final answers into the appropriate boxes in the answer sheet (marked A).
  • Open the envelopes on the START signal given by the judges. Time is measured from this moment; the winning team will be the one which finishes in the shortest total time, after any time penalties (for example for incorrect or missing answers) are applied. The time penalties are explained in each task.
  • When you have solved all the problems, hand your answer sheets to the guide, who will note the total time.
  • The maximum time available for the round is 90 minutes. After this time any remaining answer sheets should be handed in.
  • The completed answer sheets will then be marked by the jury, who will apply time penalties as appropriate. The winning team will be announced at the closing ceremony.
  • Everything you need will be provided on the table (calculator, office supplies, geometrical instruments, paper, table of constants).
  • For one of the tasks, all the screens in the room will simultaneously display a video at a specified time (the video will be repeated several times).
Table of Constants
Fundamental constants
Speed of light in vacuumcc==2.998×108 m s−12.998 \times 10^{8}\ \mathrm{m\,s^{-1}}
Planck constanthh==6.626×10−34 J s6.626 \times 10^{-34}\ \mathrm{J\,s}
Boltzmann constantkBk_B==1.381×10−23 J K−11.381 \times 10^{-23}\ \mathrm{J\,K^{-1}}
Stefan-Boltzmann constantσ\sigma==5.670×10−8 W m−2 K−45.670 \times 10^{-8}\ \mathrm{W\,m^{-2}\,K^{-4}}
Elementary chargeee==1.602×10−19 C1.602 \times 10^{-19}\ \mathrm{C}
Universal gravitational constantGG==6.674×10−11 N m2 kg−26.674 \times 10^{-11}\ \mathrm{N\,m^{2}\,kg^{-2}}
Universal electric constantϵ0\epsilon_0==8.854×10−12 m−3kg−1s4A28.854 \times 10^{-12}\ \mathrm{m^{-3}kg^{-1}s^{4}A^{2}}
Universal gas constantRR==8.315 J mol−1 K−18.315\ \mathrm{J\,mol^{-1}\,K^{-1}}
Avogadro constantNAN_\mathrm{A}==6.022×1023 mol−16.022 \times 10^{23}\ \mathrm{mol^{-1}}
Wien’s displacement constantb=λmTb = \lambda_m T==2.898×10−3 m K2.898 \times 10^{-3}\ \mathrm{m\,K}
Mass of electronmem_\mathrm{e}==9.109×10−31 kg9.109 \times 10^{-31}\ \mathrm{kg}
Mass of protonmpm_\mathrm{p}==1.673×10−27 kg1.673 \times 10^{-27}\ \mathrm{kg}
Mass of neutronmnm_\mathrm{n}==1.675×10−27 kg1.675 \times 10^{-27}\ \mathrm{kg}
Mass of Helium nucleusmHem_\mathrm{He}==6.645×10−27 kg6.645 \times 10^{-27}\ \mathrm{kg}
Atomic mass unit (a.m.u., Dalton)==1.661×10−27 kg1.661 \times 10^{-27}\ \mathrm{kg}
Astronomical data
Hubble constantH0H_0==70 km s−1 Mpc−170\ \mathrm{km\,s^{-1}\,Mpc^{-1}}
North Ecliptic Pole (J2000.0J2000.0)(αE, δE)(\alpha_\mathrm{E},\ \delta_\mathrm{E})(18h00m00s,+66∘33′39′′)(18^\mathrm{h}00^\mathrm{m}00^\mathrm{s}, +66^{\circ}33'39'')
North Galactic Pole (J2000.0J2000.0)(αG, δG)(\alpha_\mathrm{G},\ \delta_\mathrm{G})(12h51m26s,+27∘07′42′′)(12^\mathrm{h}51^\mathrm{m}26^\mathrm{s}, +27^{\circ}07'42'')
1 jansky1 Jy==10−26 W m−2 Hz−110^{-26}\ \mathrm{W\,m^{-2}\,Hz^{-1}}
1 parsec1 pc==3.086×1016 m3.086 \times 10^{16}\ \mathrm{m}
206 265 au
3.262 ly
1 astronomical unit (au)1 au==1.496×1011 m1.496 \times 10^{11}\ \mathrm{m}
1 sidereal dayTSDT_\mathrm{SD}==23.93444 h23.93444\ \mathrm{h}
23h56m04s23^\mathrm{h}56^\mathrm{m}04^\mathrm{s}
1 tropical year==365.2422 solar days
1 sidereal year==365.2564 solar days

Approximations

(1+x)n≈1+nx(1+x)^n \approx 1 + nx

(1+x)(1+y)≈1+x+y(1+x)(1+y) \approx 1 + x + y if x≪1x \ll 1 and y≪1y \ll 1

Gauss’s formulae

Spherical law of cosines: cos⁡a=cos⁡bcos⁡c+sin⁡bsin⁡ccos⁡A\cos a = \cos b \cos c + \sin b \sin c \cos A

Spherical law of sines: sin⁡Asin⁡a=sin⁡Bsin⁡b=sin⁡Csin⁡c\dfrac{\sin A}{\sin a} = \dfrac{\sin B}{\sin b} = \dfrac{\sin C}{\sin c}

next page ⟹\Longrightarrow

The Sun
Solar luminosityL⊙L_\odot==3.826×1026 W3.826 \times 10^{26}\ \mathrm{W}
Apparent angular diameter of Sunθ⊙\theta_\odot==32’
Effective temperature of SunTeff,⊙T_{\mathrm{eff},\odot}==5778 K5778\ \mathrm{K}
Apparent visual magnitude==−26.75-26.75
Absolute visual magnitude==+4.82+4.82
Apparent bolometric magnitude==−26.83-26.83
Absolute bolometric magnitude==+4.74+4.74
Distance of the Sun from the Galactic centre≈\approx8 kpc8\ kpc
The Earth and Moon
Obliquity of the ecliptic (Earth)ϵ\epsilon==23.5′23.5'
Platonic year (period of precession of Earth’s axis)==25 765 years
Apparent visual magnitude of full Moon==−12.74-12.74
Apparent angular diameter of MoonθL\theta_\mathrm{L}==31′31'
Inclination of the lunar orbit to the ecliptic==05∘08′43′′05^{\circ}08'43''
Inclination of the lunar equator to its orbital plane==6.687∘6.687^{\circ}
Lunar sidereal monthTSLT_\mathrm{SL}==27.321661 d27.321661\ \mathrm{d}
655.71986 h655.71986\ \mathrm{h}
Synodic month==29.530589d29.530589d
Tropical month==27.321582d27.321582d
Anomalistic month==27.554550d27.554550d
Draconic month==27.212221d27.212221d

The Solar System

ObjectMean radius [km]Mass [kg]Semimajor axis [au]Eccentricity
Sun695 7001.988×10301.988 \times 10^{30}——
Mercury2 4403.301×10233.301 \times 10^{23}0.3870.206
Venus6 0524.867×10244.867 \times 10^{24}0.7230.007
Earth6 3785.972×10245.972 \times 10^{24}1.0000.016 710
Moon1 7377.346×10227.346 \times 10^{22}3.844×1053.844 \times 10^{5} km0.054 900 (range 0.026−0.0770.026 - 0.077)
Mars3 3906.417×10236.417 \times 10^{23}1.5240.093
Jupiter69 9111.898×10271.898 \times 10^{27}5.2030.048
Saturn58 2325.683×10265.683 \times 10^{26}9.5370.054
Uranus25 3628.681×10258.681 \times 10^{25}19.1890.047
Neptune24 6221.024×10261.024 \times 10^{26}30.0700.009

Условие

(a) On the provided graph paper, plot the XX and YY positions of Earth and Mars in the heliocentric system over time using the data from the table, and draw vectors connecting the corresponding positions of Earth and Mars on each day.

(b) Using a ruler and set square, translate each vector to a common origin while preserving their lengths and directions. Connect the ends of the translated vectors with a curve representing the position of Mars in the geocentric system.

(c) From the plot, read off the minimal Earth–Mars distance, the duration of retrograde motion and the angle by which Mars moves backwards. Give your answers on the answer sheet.

Penalties: missing or incorrect drawing for part (b) +10 minutes; missing or out of range answers: +5 minutes for each part.

Heliocentric Equatorial Positions

EARTHMARS
DateX [au]Y [au]X [au]Y [au]
2022 Sep 010.9375−0.34311.32350.4704
2022 Sep 110.9846−0.19281.27240.5972
2022 Sep 211.0033−0.03701.20820.7178
2022 Oct 010.99280.11981.13200.8312
2022 Oct 110.95300.27311.04480.9366
2022 Oct 210.88500.41840.94771.0331
2022 Oct 310.79050.55120.84171.1200
2022 Nov 100.67220.66730.72821.1967
2022 Nov 200.53360.76310.60821.2630
2022 Nov 300.37850.83560.48301.3184
2022 Dec 100.21190.88240.35371.3628
2022 Dec 200.03870.90200.22161.3960
2022 Dec 30−0.13570.89360.08771.4182
2023 Jan 09−0.30580.8574−0.04681.4294
2023 Jan 19−0.46650.7947−0.18101.4297
2023 Jan 29−0.61280.7073−0.31391.4194
2023 Feb 08−0.74010.5981−0.44451.3988
2023 Feb 18−0.84470.4705−0.57191.3682
2023 Feb 28−0.92340.3284−0.69541.3280
2023 Mar 10−0.97400.1765−0.81401.2787
2023 Mar 20−0.99540.0191−0.92721.2207
2023 Mar 30−0.9868−0.1387−1.03411.1545
2023 Apr 09−0.9491−0.2925−1.13421.0807
2023 Apr 19−0.8835−0.4377−1.22680.9998
2023 Apr 29−0.7920−0.5702−1.31150.9124

Решение

Внимание: Непълно решение

В архива няма официално решение на тази задача.


Оригинал в Архива: team.pdf