The 1:1 mean motion resonance, or co-orbital motion, is a perfect paradigm of dynamical regime
that draws the attention of scientists belonging to different communities.
In the celestial mechanics and astrodynamics field, mathematicians, planetary scientists and aerospace engineers
study this specific three-body configuration to get a deeper understanding of the three-body problem,
to model the motion of natural bodies and eventually observe them,
and to design spacecraft trajectories for exploration missions (e.g., distant retrograde orbits or orbits associated with the Lagrangian points L3, L4 and L5).
The aim of the workshop is to bring together the three scientific commnunities to share their knowledge and experience on the co-orbital motion
as regards to mathematical tools, results and possible applications.
Workshop
Four presentations have been scheduled
COOMOT encourages the researchers to send an abstract on the following topics:
25 Feb 2022
04 Mar 2022
25 Mar 2022
Workshop Programme
but registration is required.
Day 1
10:00-10:20 Registration
10:20-10:30 Opening
10:30-11:10 A. Christou
11:15-11:35 J. Li
11:40-12:00 C. Efthymiopoulos
12:05-12:25 R. Cennamo & L. Faggioli
14:30-15:10 E. Canalias
15:15-15:35 F. Renk
15:40-16:00 G. Merisio
16:05-16:25 L. Giudici
17:00-17:20 J.D. Castro Cisneros
17:25-17:45 J. Alvarellos
Day 2
10:20-10:40 K. Oshima
10:45-11:05 B. Nicolas
11:10-11:30 G.B. Valsecchi
11:35-11:55 M. Fenucci
12:00-12:20 T. Kotoulas
14:30-15:10 A. Pousse
15:15-15:35 S. Di Ruzza
15:40-16:00 J. Palacian
16:05-16:25 M. Lara
17:00-17:20 H. Morais
17:25-17:45 Y. Huang
Day 3
10:50-11:10 R.I. Paez
11:15-11:35 F. Mokhtari
11:40-12:00 M. Giralt
12:05-12:25 V. Sidorenko
14:30-15:10 A. Leleu
15:15-15:35 J. Couturier
15:40-16:00 F. Roig
16:05-16:25 R. Moraes
17:00-17:20 A.R. Dobrovolskis
17:25-17:45 B. Gladman