Speakers and Lecture Titles

Gianni Arioli
gianni.arioli@polimi.it

Optimization of the forcing term for the solution of two point boundary value problems
Roberto Armellin
armellin@aero.polimi.it

High-order Uncertainty Management in Preliminary Orbit Determination
Edward Belbruno
belbruno@Princeton.EDU

Intriguing Solutions About a Schwarzschild Black Hole
Miguel Belló Mora
miguel.bello@deimos-space.com

Libration Point Dynamics for Lunar and Planetary Mission Design
Martin Berz
berz@msu.edu

Rigorous methods to compute flows of differential equations applied to some problems of Astrodynamics
Robert Bishop
robert.bishop@marquette.edu

Tbd
Jean-Baptiste Caillau
jean-baptiste.caillau@u-bourgogne.fr

Some results in optimal control of the restricted three-body problem
Stefano Casotto
stefano.casotto@unipd.it

On the numerical propagation of perturbations with respect to a secularly precessing elliptical orbit
Marta Ceccaroni
marta.ceccaroni@strath.ac.uk

(a) Some analytic estimates of the the Weak Stability Boundary
(b) The Weak Stability Boundary in the Sun-Jupiter-Trojan-Spacecraft four body problem

Matteo Ceriotti
matteo.ceriotti@strath.ac.uk

Plane-symmetric and Axi-symmetric Periodic Orbits in the CR3BP for Polar Earth Observation
Steven Childress
Childres@cims.nyu.edu

Camilla Colombo
camilla.colombo@strath.ac.uk

Evolution of swarms of ‘smart dust’ spacecraft
Arlin Crotts
arlin@astro.columbia.edu

The Moon as Pit Stop
Pierluigi Di Lizia
dilizia@aero.polimi.it

High Order Optimal Feedback Control of Space Trajectories
Urs Frauenfelder
frauenf@snu.ac.kr

Global surfaces of section for the planar restricted 3-body problem
Anthony Genova
Anthony.Genova@nasa.gov

Low Thrust Transfers from Sun-Synchronous Orbits to Lagrange Points and Near Earth Objects
Marian Gidea
mgidea@neiu.edu

(a) Zero-Cost Procedure to Change the Inclination of the Orbit of a Satellite near a Libration Point
(b) Weak Stability Boundaries and Invariant Manifolds

Hany Mohammed
ahamdy75@hotmail.com

Feedback optimal control of low-thrust orbit transfer in central gravity field
Nicola Hyeraci
nickh83@gmail.com

Ballistic capture in the Elliptic Restricted Three-Body Problem with Applications
Dario Izzo
Dario.Izzo@esa.int

Low-thrust interplanetary transfer as a non-linear, constrained, global optimization problem
Ruediger Jehn
Ruediger.Jehn@esa.int

Influence of Contingency Analysis on the Trajectory Design for BepiColombo
Jakub Karas
jakubkaras92@gmail.com

An Analysis of Potential Breakup and Orbital Shifts of Comet 163P/Hartley2
Jeremy Kasdin
jkasdin@Princeton.EDU

Orbital Resonances and Multiplanet Exosystems
Stephen Kemble
Stephen.KEMBLE@astrium.eads.net

Interplanetary Trajectory Optimisation exploiting multibody gravity fields
Kartik Kumar
K.Kumar@tudelft.nl

Design of a modular and robust astrodynamics toolbox
Janna Levin
janna@astro.columbia.edu

Black Holes Play Drums
Elbert Macau
elbert@lac.inpe.br

Translunar Trajectories for Low-Cost Plane Change of Terrestrial Orbits
Kyoko Makino
makino@msu.edu

Rigorous Global Optimization for Parameter Optimization using Taylor Models
Tamer Mekky
tamermekky@hotmail.com

Global Optimum Spacecraft Orbit Control in Presence of Nonlinear and Random Disturbances
Cesar Ocampo
cesar.ocampo@mail.utexas.edu

Exact Impulsive to Optimal Control Finite Burn Automation
Bart Oldeman
boldeman@encs.concordia.ca

Computing and Continuing Invariant Manifolds and Connecting Orbits in the Restricted Three Body Problem
Ashraf Owis
ahamdy75@hotmail.com

Feedback optimal control of relative motion for elliptical reference orbit of sun- facing formation flying
David Perez
perezd3@rpi.edu

Lyapunov Based Spacecraft Rendezvous Maneuver using Differential Drag
Jean-Baptiste Pomet
Jean-Baptiste.Pomet@inria.fr

On a natural distance between Keplerian ellipses
Frans Pretorius
fpretori@Princeton.EDU

Extreme limits of Black Hole Collisions
Giuliano Punzo
giuliano.punzo@strath.ac.uk

Enabling Self-similar Central Symmetry Formations
Alessandro Quarta
a.quarta@ing.unipi.it

Generalized Sail Performance in the Elliptical Restricted Three-Body Problem
Michael Reardon
mreardon@uvm.edu

A Comparison of Low Cost Transfer Orbits from GEO to LLO for a Lunar Lander Cubesat Mission
Kamesh Sankaran
ksankaran@whitworth.edu

Evaluation of Low-Thrust Propulsion Options for Cargo Missions to Near Earth Objects
Dmitry Savransky
dsavrans@princeton.edu

Parameter Distributions of Keplerian Orbits
Sven Schaeff
sven.schaeff@astos.de

Future Mission Concepts using High Power Electric Propulsion
Daniel Scheeres
scheeres@colorado.edu

Minimum Energy Configurations in the N-body Problem
Fred Singer
singer@sepp.org

Lunar origin by impact or by capture?
D. Sirbu
jkasdin@Princeton.EDU

Formation Flight for an Occulter-Based High-Contrast Imaging Mission
Paolo Teofilatto
Paolo.Teofilatto@uniroma1.it

Lunar Capture Trajectories and Homoclinic Connections through Isomorphic Mapping
Francesco Topputo
topputo@aero.polimi.it

(a) Optimal Low-Thrust, Invariant Manifold Trajectories via Attainable Sets
(b) Classification of Two-Impulse Earth--Moon Transfer

Robert Vanderbei
rvdb@Princeton.EDU

New Exotic Stable Periodic 3-Body Systems
Massimiliano Vasile
massimiliano.vasile@strath.ac.uk

Recent Advances on Methods and Techniques for Asteroid Deflection
Massimo Vetrisano
massimo.vetrisano@strath.ac.uk

Navigating to the Moon along Low-Energy Transfers: The Case of the European Student Moon Orbiter
Yang Yang
yiyinfeixiong@gmail.com

Synchronized Control for Spacecraft formation flying using State-Dependent Riccati Equation Method
Jiamin Zhu
jiamin.zhu1988@gmail.com

Quasi-periodic J2 Invariant Relative Orbits Generated from Structure-preserving Stabilization for Hamiltonian System
Federico Zuiani
fzuiani@eng.gla.ac.uk

Robust Design of Deflection Actions for Non-Cooperative Targets