session 10

2

Orbital Dispersion Simulation of Near-Earth Objects Deflection/Fragmentation by Nuclear Explosions

15'

Mr. Brian Kaplinger

Iowa State University

United States

3

Dynamics of a solar sail near a Halo orbit

15'

Dr. Ariadna Farrés

Université de Bourgogne

Spain

4

Space Trajectories for Spacecraft Re-Entry from Geostationary Orbit to Earth Using Lunar Gravity Assist

15'

Prof. Vyacheslav V. Ivashkin

Keldysh Institute of Applied Mathematics, RAS

Russian Federation

5

An improved approach to preliminary mission design using fast linear quadratic intermediate optimisations

15'

Mr. Daniel Novak

Logica Deutschland GmbH&Co. KG

Germany

6

Long-term Stable Orbits for Passive Tracking Beacon Missions to Asteroids

15'

Prof. Benjamin Villac

University of California

United States

7

Natural Ways to High Inclination Lunar Orbits

15'

Dr. Cristiano F. de Melo

Instituto Nacional de Pesquisas Espaciais (INPE)

Brazil

8

On the relationship between the Earth's Weak Stability Boundary region and the low-energy transfers to the Moon

15'

Dr. Elena Fantino

Universitat Politecnica de Catalunya (UPC)

Spain

9

Global Optimization of Transfer Orbits for Fractionated Spacecraft

15'

Dr. Lili Zheng

Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

China

10

Investigation of Semi-Major Axis Increasing for a Daily Repeat Orbit

15'

Dr. An-Ming Wu

National Space Organization

Taiwan, China

11

Solar Sail Three-Body Transfers Using Invariant Manifolds

15'

Dr. Gong Shengping

Tsinghua University

China