R. Armellin, Politecnico di Milano
Interplanetary Trajectories High-Order Guidance Based on Differential Algebra
D. Azimov, Univ. of Texas, Austin
Reconstruction of Apollo Targeting and Guidance for Powered Lunar Descent
E. Belbruno, Princeton;
F. Topputo, Politecnico di Milano
A Special Hyperbolic Invariant Set
R. Bevilacqua, US Naval Postgraduate School
Near-NonPropellant Multi-spacecraft Assembly Maneuvers by Differential Drag for LEO
G. Bignami, Italian Space Agency, President
Future Italian and European Space Programs
R. Bishop, Univ. of Texas, Austin
Improved Apollo Targeting for Onboard Lunar Landing Site Re-Designation
L. Casalino, Politecnico di Torino
Evolutionary Algorithm for Interplanetary Trajectories Optimization
C. Circi, Univ. of Rome “La Sapienza”
Analysis of Subtle Propulsion Systems for Different Mars Mission Profiles
C. Colombo, Univ. of Glasgow
An Algorithm Based on Differential Dynamic Programming for Low Thrust Trajectories
J. Condon, NASA Johnson Space Center
Trajectory Design and Performance Requirements for Human Lunar Missions
M. Dellnitz, Univ. of Paderborn
A Multiobjective Approach to Design of Low Thrust Trajectories for Spacecraft
P. DiLizia, Politecnico di Milano
Gravity Assist Space Pruning Based on Differential Algebra
N. Eismont, Russian Academy of Sciences, SRI
Solar Sails with Controllable Reflectivity as a Tool for Formation Flying
G. Fasano, Univ. of Naples
Modeling Orbital Relative Motion to enable Formation Design from Applications Requirements
R. Findlay, Univ. of Glasgow
Fuzzy Logic Control of Multi-Spacecraft Formation Flying in Elliptical Orbits
T. Fukushima, National Observatory of Japan
Efficient Numerical Integration of Rotational Motion Using Euler Parameters with Renormalization
S. Gong, Tsinghua Univ.
Formation Flying Solar-Sail Gravity Tractors in a Halo Orbit for Towing Near Earth
M. Hechler, ESA/ESOC
Orbit Design Concepts for the ESA Missions at the Libration Points
R. Jagasia, Michigan State Univ.
Validated Integration of Solar System Dynamics
Z. Kai-jian, Tsinghua Univ.
Flyby Optimization of Cassini Mission Using a Hybrid Differential Evolution
R. Kezerashvili, City Univ. of New York
The Beryllium Hollow-Body Solar Sail
K. Kumar, Delft Iniv. Of Technology
Stability of Weak Capture Trajectories
C. Maccone, IAA
The Sun as a Gravitational Lens
D. Maessen, Delft Univ. of Technology
Formation Flying Orbital Geometry of the Dutch-Chinese FAST Micro-Satellite Mission
R. Marson, Telespazio
Using Space Manifold Dynamics to Deploy a Small Telecom Constellation around the Moon
P. Massioni, Delft Univ. of Technology
Distributed Control of Space Systems Using a Decomposition Method and Linear
Matrix Inequalities
G. Mengali, Univ. of Pisa
Non-Keplerian Orbits for Electric Sail
G. Mingotti, Politecnico di Milano
A Hybrid Propulsion Approach to Design Earth-to-Moon Transfers with Ballistic Capture
M. Olle, Politecnica de Catalunya
Numerical Tools for the Computation of Homoclinic/Heteroclinic Orbits
G. Palmerini, Univ. of Rome, “La Sapienza”
Collective Control of Spacecraft Swarms for Space Exploration
P. Pergola, Alta SpA
Earth-Mars Halo to Halo Low Thrist Manifold Transfers
M. Romano, US Naval Postgraduate School
New Method to Control and Analyze with Complete Reduction the Rotation of Axially Symmetric Spacecraft
A. Rosaev, FGUP NPC “NEDRA”
Modeling of Temporary Capture onto Satellite Orbit Around Earth and Jupiter
M. Sabatini, Univ. of Rome, “La Sapienza”
Minimum Control for Spacecraft Formations in a J2 Perturbed Environment
M. Sanchez, Diemos Space SL
A Mission to Tag Asteroid Apophis
S. Zimmer, The Aerospace Corp.
Using Evolutionary Algorithms for Problems in Vast Infeasible Regions and Expensive Function Evaluations