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Showing posts with label 2019 QR6. Show all posts
Showing posts with label 2019 QR6. Show all posts

Monday, December 30, 2019

Amors: (2019 QR6) and (2019 PR2) - investigation about cometary origin

These two asteroids have similar orbital parameters.
A possibility that should be investigated is that these asteroids separated recently from a common body ... see previous posts for a draft analysis.

Another aspect is that they might have a cometary origin.

For what's worth, considering the uncertainty (orbit condition code 4) and considering that I do not take into account non gravitational effects, I made a backward simulation with 2019 PR2

2019 PR2
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 47 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7976773108833863 1.3756e-05  
a 5.772423469462186 0.00040358 au
q 1.167892239061442 2.2478e-06 au
i 10.98950352005738 9.7173e-05 deg
node 349.038132037726 0.00014302 deg
peri 57.08261419342178 0.00010673 deg
M 347.1019573973371 0.0013592 deg
tp 2458781.991800392675
(2019-Oct-25.49180039)
9.5194e-05 TDB
period 5065.656096365621
13.87
0.53125
0.001454
d
yr
n .07106680618494488 7.453e-06 deg/d
Q 10.37695469986293 0.00072551 au
  Orbit Determination Parameters
   # obs. used (total)      215  
   data-arc span      139 days  
   first obs. used      2019-08-10  
   last obs. used      2019-12-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .40041  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-28 08:29:27  

Additional Information
 Earth MOID = .236158 au 
 Jupiter MOID = .430847 au 
 T_jup = 2.149 


Clones
I generated 100 clones trying to achieve the same orbital parameters as calculated by JPL Small Body Database

Clones  Target
mean sd   mean sd
q 1.16789207 2.25e-06   1.16789224 2.25e-06
e 0.79767637 1.375e-05   0.79767731 1.376e-05
i 10.98949691 9.732e-05   10.98950352 9.717e-05
peri 57.08261449 0.00010684   57.08261419 0.00010673
node 349.03812785 0.00014309   349.03813204 0.00014302
tp 2458781.99180559 9.518e-05   2458781.99180039 9.519e-05


Simulation
Mercury6 simulator was set up like this (param.in file):



)---------------------------------------------------------------------
) Important integration parameters:
)---------------------------------------------------------------------
 algorithm (MVS, BS, BS2, RADAU, HYBRID etc) = BS
 start time (days)= 2458849.5
 stop time (days) = -1d8
 output interval (days) = 100
 timestep (days) = 0.05
 accuracy parameter=1.d-12
...
ejection distance (AU)= 1d2

As shown above, the arbitrary threshold to declare  that a clone has a cometary origin is set to 100 AU
I take into account all planets plus asteroids Ceres, Pallas and Vesta.

Simulation results 
At the end of the simulation, we find:
  • 72 out of 100 clones were ejected from the solar system
  • 2 out of 100 clones "hit" the sun

Considering that the simulation is backward in time, the above results must be read as:
  • 72 out of 100 clones have a cometary origin (they entered the solar system from a distance greater that 100 AU)
  • 2 out of 100 clones seem to have originated from the sun ! (we have to discard these as impossible results)

The following plots have been done using R scripts and package ggplot2.

First of all, we can see that there is not a "single" point in time when the clones likely to have a cometary origin have entered the solar system even though the are slightly more concentrated around 29000 years ago


Distribution of min perihelium
The simulation time has been divided into 10 slots.
In every slot, for every asteroid, we calculate the minimum perihelium that it had during that period.
The various values  are shown in a boxplot.
A similar approach is used for all the other plots. 

Distribution of max aphelium
Some clones entered the solar system on a hyperbolic trajectory, it does not make sense to calculate an aphelium (infinite) so they are not shown here:

... ooops!, an outlier ... if we omit it we have a better idea ... actually, we have to omit them about a dozen times before seeing something:

Distribution of max Orbital Period
...again after omitting several outliers:

Distribution of max Orbital Energy
In this graph, those clones with orbital energy >0 are on a hyperbolic orbit:

Distribution of Vinfinity
For those asteroids having an hyperbolic trajectory, it make sense to plot their Vinfinity:


Distribution of max eccentricity




References

Mercury6 simulator:
J.E.Chambers (1999) ``A Hybrid
      Symplectic Integrator that Permits Close Encounters between
      Massive Bodies''. Monthly Notices of the Royal Astronomical
      Society, vol 304, pp793-799.

package R:
  R Core Team (2019). R: A language and environment for statistical
  computing. R Foundation for Statistical Computing, Vienna, Austria.
  URL https://www.R-project.org/.

package ggplot2:
  H. Wickham. ggplot2: Elegant Graphics for Data Analysis.
  Springer-Verlag New York, 2016.




Cheers,
Alessandro Odasso