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UID:pretalx-juliacon2024-SQFY3B@pretalx.com
DTSTART;TZID=CET:20240710T164000
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DESCRIPTION:One of the main problems in the computation of orbital predicti
 ons\, is the propagation of the orbital uncertainty. This problem is relev
 ant in a wide range of scenarios\, from the design of interplanetary space
 craft trajectories\, to the assessment of the hazard posed by an asteroid 
 impacting the Earth. In this talk\, we present a technique to propagate la
 rge sets of initial conditions in TaylorIntegration.jl via a technique cal
 led Automatic Domain Splitting (ADS).
DTSTAMP:20260305T203734Z
LOCATION:While Loop (4.2)
SUMMARY:Propagating large orbital uncertainty with TaylorIntegration.jl - J
 orge A. Pérez-Hernández\, Luis Eduardo Ramírez Montoya\, Luis Benet
URL:https://pretalx.com/juliacon2024/talk/SQFY3B/
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