The CFEPS Kuiper Belt Survey: Strategy and presurvey results

被引:49
作者
Jones, R. L.
Gladman, B.
Petit, J-M
Rousselot, P.
Mousis, O.
Kavelaars, J. J.
Bagatin, A. Campo
Bernabeu, G.
Benavidez, P.
Parker, J. Wm.
Nicholson, P.
Holman, M.
Grav, T.
Doressoundiram, A.
Veillet, C.
Scholl, H.
Mars, G.
机构
[1] Univ British Columbia, Dept Phys & Astron, Vancouver, BC V6T 1Z1, Canada
[2] Observ Besancon, F-25010 Besancon, France
[3] Univ Alicante, Dept Fis Ingn Sistemas & Teor Senal, EPSA, E-03080 Alicante, Spain
[4] SW Res Inst, Dept Space Studies, Boulder, CO 80302 USA
[5] Cornell Univ, Dept Astron, Ithaca, NY 14853 USA
[6] Harvard Smithsonian Ctr Astrophys, Cambridge, MA 02138 USA
[7] Univ Hawaii, Inst Astron, Honolulu, HI 96822 USA
[8] Observ Paris, Lab Etud Spatiales & Instrumentat Astrophys, F-92195 Meudon, France
[9] Canada France Hawaii Telescope Corp, Kamuela, HI 96743 USA
[10] Observ Cote Azur, F-06304 Nice 4, France
关键词
trans-neptunian objects; Kuiper belt objects;
D O I
10.1016/j.icarus.2006.07.024
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
We present the data acquisition strategy and characterization procedures for the Canada-France Ecliptic Plane Survey (CFEPS), a sub-component of the Canada-France-Hawaii Telescope Legacy Survey. The survey began in early 2003 and as of summer 2005 has covered 430 square degrees of sky within a few degrees of the ecliptic. Moving objects beyond the orbit of Uranus are detected to a magnitude limit of m (R) = 23-24 (depending on the image quality). To track as large a sample as possible and avoid introducing followup bias, we have developed a multi-epoch observing strategy that is spread over several years. We present the evolution of the uncertainties in ephemeris position and orbital elements of a small 10-object sample of objects tracked through these epochs as part of a preliminary presurvey starting a year before the main CFEPS project. We describe the CFEPS survey simulator, to be released in 2006, which allows theoretical models of the Kuiper belt to be compared with the survey discoveries. The simulator utilizes the well-documented pointing history of CFEPS, with characterized detection efficiencies as a function of magnitude and rate of motion on the sky. Using the presurvey objects we illustrate the usage of the simulator in modeling the classical Kuiper belt. The primary purpose of this paper is to allow a user to immediately exploit the CFEPS data set and releases as they become available in the coming months. (c) 2006 Elsevier Inc. All rights reserved.
引用
收藏
页码:508 / 522
页数:15
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