session 7

Title

Orbital Dynamics (2)

Description

This theme discusses advances in orbital dynamics, orbit determination, and orbit control. It includes orbital dynamics associated with constellations and formation flying.

Date

2012-10-04

Time

15:15

Room

TS01 (Sala Aldebaran, Hall 1)

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Low-Energy Earth-Moon Transfers Involving Manifolds via Isomorphic Mapping

accepted

15'

confirmed

Dr. Mauro Pontani

Sapienza University of Rome

Italy

2

Representations of Higher-Dimensional Poincare Maps with Applications to Spacecraft Trajectory Design

accepted

15'

confirmed

Ms. Amanda Haapala

Purdue University

United States

3

Progress in Solving the “Unsolved Problems in Satellite Theory”

accepted

15'

confirmed

Dr. David Finkleman

International Organization for Standardization

United States

4

Spatial Approaches to Moons from Resonance Relative to Invariant Manifolds

accepted

15'

confirmed

Dr. Rodney Anderson

Jet Propulsion Laboratory - California Institute of Technology

United States

5

Low-Energy Cislunar and Trans-lunar Transfer Trajectories from the View of Libration Points

accepted

15'

confirmed

Dr. Ming Xu

Beihang University

China

6

Analytical perturbative theories of motion in highly inhomogeneous gravitational fields

accepted

15'

confirmed

Dr. marta ceccaroni

University of Strathclyde

Italy

7

Averaged model to analyze the long-term orbital evolution of the binary asteroid

accepted

15'

confirmed

Mr. Xiaodong Liu

Tsinghua University

China

8

Analytical Solution of the Third-Body Problem for Highly Elliptical Orbits Based on the Time-Dependent Lie-Deprit Transform

accepted

15'

withdrawn

Mr. Guillaume LION

University of Nice-Sophia Antipolis, CNRS, Observatoire de la Cote d'Azur

France

9

Study of resonances due to third body perturbations in the dynamics of MEOs

accepted

15'

confirmed

Dr. Letizia Stefanelli

University of Nice-Sophia Antipolis, Observatoire de la Cote d'Azur, CNES

France

10

Optimal Low-Cost Transfer Transfer to L4 and L5 Lagrangian points based on the G-Family of Periodic Orbits

accepted

15'

confirmed

Prof. Elbert E.N. Macau

Instituto Nacional de Pesquisas Espaciais (INPE)

Brazil

11

A new description of planet-to-planet transfer in alternating rotating coordinate with applications

accepted

15'

confirmed

Mr. Jun Matsumoto

The University of TOKYO, Graduate school

Japan

12

Effects of the Atmospheric Drag in Close Approaches for a Cloud of Particles

accepted

15'

confirmed

Dr. Antonio Prado

National Institute for Space Research - INPE

Brazil

13

High-Accuracy Asymmetric Circumlunar Free Return Trajectory Design with High-Latitude Landing for China

accepted

15'

confirmed

Mr. Shing Yik Yim

Tsinghua University

China