session 5

Title

Mission Design, Operations and Optimisation (2)

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

2012-10-03

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

Design of trajectories for continuous polar Earth observation in the Earth-Moon system

accepted

15'

confirmed

Dr. Matteo Ceriotti

University of Glasgow

United Kingdom

2

Innovative method of constellation design to enable new arising applications based on space-airborne bistatic SAR

accepted

15'

confirmed

Dr. Maria Daniela Graziano

CO.RI.S.T.A./Second University of Naples

Italy

3

Optimization of Satellite Constellation Reconfiguration Maneuvers

accepted

15'

confirmed

Mr. Leonid Appel

Technion, I.I.T.

Israel

4

A predictive guidance scheme for soft landing of a lunar module

accepted

15'

confirmed

Mr. Nitin Ghatpande

Indian Space Research Organization (ISRO)

India

5

An extension and numerical analysis of the hohmann spiral transfer

accepted

15'

confirmed

Mr. Steven Owens

Advanced Space Concept Laboratory, University of Strathclyde

United Kingdom

6

MESSENGER at Mercury: From Orbit Insertion to First Extended Mission

accepted

15'

confirmed

Mr. James V. McAdams

Johns Hopkins University Applied Physics Laboratory

United States

7

Orbit selection criteria for optical dual-use earth observation satellites

accepted

15'

confirmed

Mr. Alessio Di Salvo

NEXT Ingegneria dei Sistemi S.p.A.

Italy

8

Optimal Trajectory Design for the Lunar Vertical Landing

accepted

15'

confirmed

Dr. Dong-Hyun Cho

KARI

Korea, Republic of

9

Optimal Long-duration Low-thrust Transfers Between Libration Point Orbits

accepted

15'

confirmed

Dr. Richard Epenoy

Centre National d'Etudes Spatiales (CNES)

France

10

Optimal Spacecraft Trajectories for Flight to Asteroid Apophis with Low Thrust

accepted

15'

confirmed

Prof. Vyacheslav V. Ivashkin

Keldysh Institute of Applied Mathematics, RAS

Russian Federation

11

A novel approach to the generation of multiple gravity assist trajectories

accepted

15'

withdrawn

Dr. Elena Fantino

Universitat Politecnica de Catalunya (UPC)

Spain

12

Low energy trajectory optimization for CE-2’s extended mission after 2012

accepted

15'

confirmed

Dr. Mingtao Li

National Space Science Center (NSSC), Chinese Academy of Sciences

China

13

Gravitational Capture Opportunities for Asteroid Retrieval Missions

accepted

15'

confirmed

Dr. Joan Pau Sanchez Cuartielles

Advanced Space Concept Laboratory, University of Strathclyde

United Kingdom