Speakers and Lecture Titles



Countries Represented: Denmark, Israel, Italy, France, Germany, Netherlands, Russia, Scotland, Spain, Sweden, United States

Kyle T. Alfriend

Department of Aerospace Engineering
Texas A&M University

alfriend@aero.tamu.edu

Challanges in Maintaining a Large Space Object Catalog

J. J. Arrieta-Camacho; L. T. Biegler

Space Systems Engineering
Carnegie Mellon University

jarrieta@andrew.cmu.edu

A Framework for the Design, Analysis, and Optimization of Earth-Moon Trajectories

Neil Ashby

Department of Physics
University of Colorado

ashby@boulder.nist.gov

Relativistic Planetary Perturbation Equations with Velocity-Dependent Forces

Edward Belbruno

Department of Astrophysical Sciences, Princeton University, and
Innovative Orbital Design, Inc.

belbruno@math.princeton.edu

Slow Chaotic Transfer Between Planetary Systems

Srinivas Bettadpur

Aerospace Engineering and Engineering Mechanics
University of Texas at Austin

srinivas@csr.utexas.edu

Precision Orbit Determination for LEO Satellites - GRACE Case Study

J. Bickford(1); et al

Draper Laboratory
Cambridge, MA

jbickford@draper.com

Natural Sources of Antiparticleds in the Solar System, and the Feasibility of Extraction die High Delta-V Space Propulsion

Robert Bishop; Dilmurat Asimov

Department of Aerospace Engineering & Engineering Mechanics
The University of Texas at Austin

rhbishop@mail.utexas.edu

Analysis of Planetary Re-Entry Vehicles with Spiraling Motion

Mickael Chekroun

Environmental Research and Teaching Institute, Ecole Normale Superieure
Institut Polytechnique des Sciences Avancees, France

chekro@lmd.ens.fr

On the Stability of Periodic Orbits: Floquet Theory Revisited

Edgar Choueiri

Department of Mechanical and Aerospace Engineering
Princeton University

choueiri@princeton.edu

Using Radio-frequency Waves to Propel Spacecraft: Electrodeless Concepts in Plasma Propulsion

Douglas Currie

Department of Physics
University of Maryland

currie@umd.edu

The Role of Thermal Thrust. WeberSat and the Lense-Thirring Effect

Michael Dellnitz; Kathrin Padberg; Bianca Thiere; Marcus Post

Faculty of Computer Science, Electrical Engineering and Mathematics
University of Paderborn, Germany

dellnitz,padberg,thiere@math.upb.de

Set Oriented Numerics in Astrodynamics

J.R.C. Demeyeri(1); Pini Gurfil(2)

(1)Faculty of Aerospace Engineering, Delft University of Technology
(2)Faculty of Aerospace Engineering, Technion - Israel Insitute of Technology

J.R.C.Demeyer@student.tudelft.nl

Transfer from Earth to Distant Retrograde Orbits using the Hyperbolic Network Around L1

Irah Donner

Wilmer Cutler Pickering Hale and Dorr LLP, Senior Partner
New York City

Irah.Donner@wilmerhale.com

Patents: A Necessary Evil?!

David Dunham

APL(Johns Hopkins University)
Baltimore, MD

David.Dunham@jhuapl.edu

Mission Design for STEREO and for Other Operating APL Spacecraft

Michael Efroimsky(1); Valery Lainey(2)

(1) US Naval Observatory
(2) L'Observatoire de Paris

efroimsky.michael@usno.navy.mil

On the Theory of Bodily Tides. The Models and the Physics

Antonio Elipe

Grupo de Mecanica Espacial
University of Zaragoa

elipe@unizar.es

Equilibria and Bifurcations in the Rotation of a Gyrostat

David C. Folta

NASA Goddard Space Flight Center
Greenbelt, Maryland

david.folta@gsfc.nasa.gov

Innovative Trajectory Designs to meet Exploration Challanges

Marian Gidea

Department of Mathematics
Northeastern Illinois University

mgidea@neiu.edu

Geometry of Homoclinic Connections in a Planar Circular Restricted Three-Body Problem
Paul A. Gilster

Writing on Technology and Its Implications
Raleigh, North Carolina

gilster@mindspring.com

TBD
Pini Gurfil

Department of Aerospace Engineering
Technion - Israel Institute of Technology
Israel

pgurfil@technion.ac.il

On Guage Symmetry in Finite-Dimensional Dynamical Systems

Kathleen Howell

School of Aeronautics and Astronautics
Purdue University

Howell@purdue.edu

A Representation of Invariant Manifolds for Trajectory Design
Gerald P. Jackson

Hbar Technologies, LLC

gjackson@hbartech.com

Instellar Transport Using Nuclear Sails
Les Johnson; Edward E. Montgomery IV

NASA George C. Marshall Space Flight Center

Charles.L.Johnson-1@nasa.gov

Status of Solar Sail Propulsion - Moving Toward an Instellar Probe

Jordin T. Kare

Kare Technical Consulting

jtkare@attglobal.net

Sailbeam/Magsail: Practical Propulsion for 0.1c Interstellar Rendezvous Probes

Egemen Kolemen; Jeremy Kasdin; Pini Gurfil

Mechanical and Aerospace Engineering
Princeton University

ekolemen@princeton.edu

Quasi-Periodic Orbits of the Restricted Three-Body Problem Made Easy

Sergei Kopeikin

Department of Physics and Astronomy
University of Missouri

kopeikins@missouri.edu

Relativistic Navigation in the Solar System

Martin Lo

Jet Propulsion Laboratory

martin.lo@jpl.nasa.gov

Orbital Study for Planet Finding with Occulters

Claudio Maccone

International Academy of Astronautics
Italy

clmaccon@libero.it

Sun's Focus Comes First, Interstellar Target Comes Second

Christie Maddock

Department of Aerospace Engineering
University of Glasgow, Scotland

c.maddock@aero.gla.ac.uk

Comparison of single and multi-spacecraft configurations for NEA deflection by solar sublimation

Gregory L. Matloff

(1)Department of Physical and Biological Sciences
New York City Technical College, CUNY

gregmat@hotmail.com

Interim Missions for Photon Sailcraft: How to Prep for Centaurus

Mark G. Millis

NASA John H. Glenn Research Center at Lewis Field
Cleveland, Ohio
and
Tau Zero Foundation

marc.g.millis@nasa.gov

Incessant Obsolescence Postulate and 'Practical' Interstellar Flight

Greg Olsen

GHO Ventures, LLC
Princeton

golsen@ghoventures.com

Entrepreneur and Scientist in Space

Ashraf Owis

Mathematics
Milano-Bicocca University

ashraf.owis@unimib.it

Optimal Feedback Control in Interplanetry Space Missions

Jesus Palacian; Patricia Yanguas

Matematica e Informatica
Universidad Publica de Navarra

palacian@unavarra.es
yanguas@unavarra.es

The Normally Hyperbolic Invariant Manifolds of the Collinear Points of the Restricted Three-Body Problem

Ryan S. Park; D.J. Scheeres

Department of Aerospace Engineering
The University of Michigan
Ann Arbor, MI

scheeres@umich.edu
sanghp@umich.edu

,
Nonlinear Bayesian Estimation for Spacecraft Trajectory and Navigation

Erricos Pavlis(1); Ignazio Ciufolini(2)

(1)Joint Center for Earth Systems Technology
University of Maryland - Baltimore County
(2)Universita' di Lecce, Italy

epavlis@umbc.edu

Space geodetic experiments for fundamental physics. Frame-dragging observed with Satellite Laser Ranging

John Pazmino

NYSkies Astronomy Inc, and
National Space Society

nyskiesastronomy@earthlink.net

Gravity Behaves Like That?

Mason Peck

Cornell University

mp336@cornell.edu

Very Small Interstellar Spacecraft

John Remo

Harvard University
Department of Astronomy
Cambridge, MA

jremo@cfa.harvard.edu

Defining Characeristics of Planets

Shane Ross

Department of Engineering Science and Mechanics
Virginia Polytechnic Institute and State University

sdross@vt.edu

Multiple Gravity Assists in the Restricted Three-Body Problem

V.V.Sidorenko(1); S. Skorokhod(2)

(1)Keldysh Institute of Applied Mathematics, Moscow, Russia
(2)Moscow Institute of Physics and Technology, Russia

sidorenk@spp.keldysh.ru

Re-entry Dynamics of Uncontrolled Mars Probe

S. Fred Singer

Science and Environmental Policy Project
Arlington, VA

singer@sepp.org

Capture Mechanisms for the Origin of the Moon

John Slough

Plasma Dynamics Laboratory
University of Washington

slough@aa.washington.edu

Near Term Fusion Based on Small Scale, High Efficiency Reactor

Francesco Topputo; Giorgo Mingoyyi; Franco Bernelli-Zazzera

Dipartimento di Ingegneria Aerospaziale
Politecnico di Milano - Campus Bovisa
Italy

topputo@aero.polimi.it

Low Thrust, Stable Manifold Trajectories to Halo Orbits

Lee Valentine

Space Studies Institute

lsvalentine@verizon.net

Critical Trajectories for the Human Settlement of the High Frontier

Robert Vanderbei; Egeman Koleman

Princeton University

rvdb@princeton.edu

Linear Stability of Ring Systems

Massimiliano Vasile

Aerospace Engineering; University of Glasgow

mvasile@aero.gla.ac.uk

A Multicriteria Assessment of Some Deflection Methods for Dangerous NEOs

Dimitri Veras

Department of Astrophysical and Planetary Sciences
University of Colorado at Boulder

dveras@gmail.com

A resonant term-based integrator including effects from a nascent disk, precession, oblateness, and general relativity