session 3

Title

Orbital Dynamics - Part 1

Description

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

Date

2011-10-04 15:00

Room

TS-04

IPC members
papers

Order

Presentation status

Mode

Paper title

Main author

Affiliation

Country

1

confirmed

Effect of a drag force due to absorption of solar radiation on solar sail orbital dynamics

Prof. Roman Ya. Kezerashvili

New York City College of Technology

United States

2

confirmed

Analytical Solutions of the Relative Motion About a Keplerian Elliptic Orbit

Prof. Gerard Gomez

University of Barcelona

Spain

3

confirmed

Post-aerocapture orbit selection and maintenance for the Aerofast mission to Mars

Dr. Mauro Pontani

University of Rome “La Sapienza”

Italy

4

confirmed

An Extended Discussion on the DoubleStar Orbits

Dr. Jingshi Tang

Nanjing University

China

5

confirmed

Station keeping of a solar sail in the solar system

Dr. Ariadna Farrés

Université de Bourgogne

Spain

6

withdrawn

India's first MARS Mission Orbit Determination System

Dr. Narayanasetti Venkata Vighnesam

Indian Space Research Organization (ISRO)

India

7

confirmed

Optimal Impulsive Orbital Maneuver between Noncoplanar Noncoaxial orbits with or without Time constraint

Prof. M. Navabi

Shahid Beheshti University

Iran

8

confirmed

Natural Periodic Relative Orbit Solving using Fourier Series

Dr. Jing Cao

College of Astronautics,Northwestern Polytechnical University

China

9

confirmed

Long-term evolution of Galileo operational orbits by canonical perturbation theory

Dr. Martin Lara

Spain

10

confirmed

Simulation of Orbit and Guidance Design for TSLV

Prof. Rock Jeng-Shing Chern

University of Science & Technology

Canada

11

confirmed

Stability analysis of a highly eccentric orbit around Mars

Mrs. Bannihatti Parameshwarappa Dakshayani

ISRO Satellite Centre (ISAC)

India

12

withdrawn

Mars-Phobos low energy transfer in the restricted three body problem

Dr. Dong Qiao

Beijing Institute of Technology

China