OpenOrb: Open-source asteroid orbit computation software including statistical ranging

被引:54
作者
Granvik, Mikael [2 ]
Virtanen, Jenni [1 ]
Oszkiewicz, Dagmara [3 ]
Muinonen, Karri [3 ]
机构
[1] Finnish Geodet Inst, Masala 02431, Finland
[2] Univ Hawaii, Inst Astron, Honolulu, HI 96822 USA
[3] Univ Helsinki, FIN-00014 Helsinki, Finland
关键词
IDENTIFICATION;
D O I
10.1111/j.1945-5100.2009.tb01994.x
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
0708 ; 070902 ;
摘要
We are making an open-source asteroid orbit computation software package called OpenOrb publicly available. OpenOrb is built on a well-established Bayesian inversion theory. which means that it is to a large part complementary to orbit-computation packages Currently available. In particular, OpenOrb is the first package that contains tools for rigorously estimating the uncertainties resulting from the inverse problem of computing orbital elements using scarce astrometry. In addition to the well-known least-squares method, OpenOrb also contains both Monte-Carlo (MC) and Markov-Chain MC (MCMC; Oszkiewicz et al. [2009]) versions of the statistical ranging method. Ranging allows the user to obtain sampled, non-Gaussian orbital-element probability-density functions and is therefore optimized for cases where the amount of astrometry is scarce or spans a relatively short time interval. Ranging-based methods have successfully been applied to a variety of different problems such as rigorous ephemeris prediction, orbital element distribution Studies for transneptunian objects, the computation of invariant collision probabilities between near-Earth objects and the Earth, detection of linkages between astrometric asteroid observations within an apparition as well as between apparitions, and in the rigorous analysis of the impact of orbital are length and/or astrometric uncertainty on the uncertainty of the resulting orbits. Tools for making ephemeris predictions and for classifying objects based on their orbits are also available in OpenOrb. As an example, we use OpenOrb in the search for candidate retrograde and/or high-inclination objects similar to 2008 KV42 in the known population of transneptunian objects that have an observational time span shorter than 30 days.
引用
收藏
页码:1853 / 1861
页数:9
相关论文
共 21 条
[1]  
BOWELL E, 1993, B AM ASTRON SOC, V25, P1118
[2]  
Danby J., 1992, Fundamentals of Celestial Mechanics
[3]  
Decyk VK., 1997, Introduction to Object-Oriented Concepts using Fortran90
[4]   DISCOVERY OF THE FIRST RETROGRADE TRANSNEPTUNIAN OBJECT [J].
Gladman, B. ;
Kavelaars, J. ;
Petit, J. -M. ;
Ashby, M. L. N. ;
Parker, J. ;
Coffey, J. ;
Jones, R. L. ;
Rousselot, P. ;
Mousis, O. .
ASTROPHYSICAL JOURNAL LETTERS, 2009, 697 (02) :L91-L94
[5]   Asteroid identification at discovery [J].
Granvik, M ;
Muinonen, K .
ICARUS, 2005, 179 (01) :109-127
[6]   Transneptunian Object Ephemeris service (TNOEPH) [J].
Granvik, M ;
Virtanen, J ;
Muinonen, K ;
Bowell, E ;
Koehn, B ;
Tancredi, G .
EARTH MOON AND PLANETS, 2003, 92 (1-4) :73-78
[7]   Asteroid identification over apparitions [J].
Granvik, Mikael ;
Muinonen, Karri .
ICARUS, 2008, 198 (01) :130-137
[8]   AN INVARIANT FORM FOR THE PRIOR PROBABILITY IN ESTIMATION PROBLEMS [J].
JEFFREYS, H .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1946, 186 (1007) :453-461
[9]  
Lehtinen M., 1988, PITMAN RES NOTES MAT, V167, P46
[10]   The asteroid identification problem - I. Recovery of lost asteroids [J].
Milani, A .
ICARUS, 1999, 137 (02) :269-292