Variants of the La2010 solutions.
|La2010a||ast5AL08cxc||INPOP08a||0.58 Myr||1 × 10-3||Ext||5ast,M|
|La2010a*||ast5AL08czc||INPOP08a||0.58 Myr||0.9765625 × 10-3||Ext||5ast,M|
|La2010b||ast5AL08cx||INPOP08a||0.58 Myr||5 × 10-3||Ext||5ast,M|
|La2010b*||ast5AL08cz||INPOP08a||0.58 Myr||4.8828125 × 10-3||Ext||5ast,M|
|La2010c||ast0AL08cx2a||INPOP08a||1 Myr||5 × 10-3||Ext||0ast,M|
|La2010c*||ast0AL08cz2a||INPOP08a||1 Myr||4.8828125 × 10-3||Ext||0ast,M|
|La2010d||ast5ALix||INPOP06||1 Myr||5 × 10-3||Ext||5ast,M|
Notes. The nominal solution La2010a is obtained for a stepsize τ = 1 × 10-3 in extended precision. The other solutions with different settings have been computed to test the stability of the nominal solution. The column “files” denotes the name of the computer files of the solution, “ephem” is the name of the reference INPOP ephemeris, “fit” is the time length of the ephemeris used for the fit, and τ is the step size of the numerical integration. In “prec”, Ext indicates that the integration was performed in extended precision. In the last column, 5ast indicates that five asteroids have been integrated, and M stands for the Moon as a separate object.
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