session 4

Title

Mission Design, Operations and Optimisation (1)

Description

The theme covers design, operations and optimisation of Earth-orbiting and interplanetary missions, with emphasis on studies and experiences related to current and future missions.

Date

2012-10-02

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

SYMPOSIUM KEYNOTE: Expansion of our Sphere of activity with Astrodynamics and cutting edge Technology

accepted

30'

confirmed

Dr. Junichiro Kawaguchi

Japan Aerospace Exploration Agency (JAXA)

Japan

2

Hybrid low-thrust transfers to eight-shaped orbits for polar observation

accepted

15'

confirmed

Dr. Jeannette Heiligers

University of Strathclyde

United Kingdom

3

Enhancing Planetary Exploration by Using Hybrid Propulsion Transfers

accepted

15'

confirmed

Dr. Francesco Topputo

Politecnico di Milano

Italy

4

Preliminary Study of the Trajectory from the Earth to the Moon with Low thrust for the Small Scientific Spacecraft, DESTINY

accepted

15'

confirmed

Dr. masaki nakamiya

Kyoto University

Japan

5

Low-thrust Interplanetary Transfer Design by Evolving Freeform Artificial Neural Networks

accepted

15'

withdrawn

Dr. Shuguang Li

Northwestern Polytechnical University

China

6

Extension of Finite Perturbative Elements for Multi-Revolution Low-Thrust Transfer Optimisation

accepted

15'

confirmed

Mr. Federico Zuiani

University of Glasgow, Space Advanced Research Team

United Kingdom

7

Mission analysis and orbit control strategy for a space mission on a polar tundra orbit

accepted

15'

confirmed

Ms. Valentina Boccia

Università degli Studi di Napoli “Federico II”

Italy

8

High Area-to-Mass Ratio Hybrid Propulsion Earth to Moon Transfers in the CR3BP

accepted

15'

confirmed

Mr. Willem van der Weg

University of Strathclyde

United Kingdom

9

Mission Design and Analysis for the DEIMOS-2 Earth Observation Mission

accepted

15'

confirmed

Ms. Stefania Cornara

Deimos Space S.L.

Spain

10

Particle Swarm Optimization of Ascending Trajectories of Multistage Rockets

accepted

15'

confirmed

Dr. Mauro Pontani

Sapienza University of Rome

Italy

11

Optimization of lunar soft landing trajectory based on hybrid method

accepted

15'

withdrawn

Mr. Tao Cao

Shanghai Aerospace Control Engineering Institute

China

12

Constellations of inclined heliotropic orbits for enhanced Earth coverage

accepted

15'

confirmed

Dr. Camilla Colombo

University of Southampton

Italy