peter vereš, juraj tóth, leonard kornoš search for very close approaching neas comenius...
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Peter Vereš, Juraj Tóth, Leonard Kornoš
Search for very close approaching Search for very close approaching NEAsNEAs
Comenius University, Bratislava, Slovakia
Faculty of mathematics, physics and informatics
Department of astronomy, physics of the Earth and meteorology
Objectives
• Create NEA model population
• Simulation of geometrical conditions during close Earth encounters
• Detection probability of synthetic population
Known NEA population
NEA NEC PHO IEO
05/01/2006 3769 77 774 5
Size depending on
avg. A
Known population
Bottke model
2001
Rabinowitz model
1994
Stuart model
2004
D>1000m 95% 73% 71%
D>100m 8,7% 3,2% 3,2%
D>10m
253137302614383747
55.10 % 510 % 43.10 %
5020750
• Known NEO counts versus models
Known NEA population• Orbital elements & size distribution of NEA
• Smaller NEAs – lesser count
• Closest approaches to the Earth within Moon orbit distance & their size distribution
Survey programs
1 25log( ) 2.5log 1V r H G G
0.63
1 exp 3.33tan2
1.22
2 exp 1.87 tan2
120
0,15;0,40G
10 105log 2,5logH C D A
Apparent magnitude
Absolute magnitude – Albedo - Size
Our work: 18m – 1kmalbedo vs. diameter 23m – 100m
28m – 10m
Limiting conditions:
WFS• Idea to search in the close Earth vicinity, wide field vs. low limit. mag.
WFS: f=0,15m 0,18m 15°2 14m 450°/h 30sLINEAR: f=2,2m 1,00m 2°2 20m 210°/h 5s
WFS limitations
Creating model populationRandom number generation according to distributions a, e, i, H
N bodies – each contains 6 orbital elements, size (H)
NEO space correction
Angular elements – random seed
Generation accuracy
10 964 780 synthetic bodies
Numerical integration
Numerical integrator (Montebruck-Pfleger)
JPL database DE406 (accuracy +3000years = ~25m in planets orbits)
Multistep backward integration of Adams-Bashforth-Moulton type
Perturbing elements vs. Keplerian motion, 12-grade of accuracy
Reduction: only Sun & Earth perturbing
Input (name, MJD, a, e, i,, , v, H)
Output (name, MJD, , R, h, Ph, RA, DC )
Integration time 1 year
Output conditions: V<14m a (mean Earth-Moon distance)
Results reduction for WFS
30
• Possible discoveries for H>19 bodies + visual mag. condition = 18 discoveries
• For H>19, >0,46AU, , angular velocity limiting magnitude correction
for WFS, site of observation – declination restriction, obs. time restriction = 3,6
– 5,4 discoveries
• Analyzing each encounter as real (real time and date, RA & DA, time spent
inside search area ) = 3,35 discoveries
• Synthetic asteroid No. 2 961 437 collides with the Earth 25,6 ~ 26H D m
• 80 NEA inside Moon orbit annually
• 18 NEA are capable to find under ideal conditions annually with WFS
• 3 NEA are easily to find with WFS Modra annually
• Optimistic models expect up to 120 discoveries with WFS
• Limiting magnitude +18m & preserving wide field expect rapid number of
discoveries in the close Earth vicinity
• High angular motion is expected
Final results
1 60 '/ min
Future
• Actual & accurate models
• Higher number of integrated orbits – bodies down to bolid size (1 meter)
• Longer integration time – fluctuations and orbits perturbation due to close
encounters
• Build of WFS, discoveries & confirmation of our model and other models
• Upgraded survey system with +18m limit magnitude