session 2

Title

Guidance, Navigation and Control (2)

Description

The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft and rockets, including rendezvous and docking.

Date

2012-10-02

Time

10:15

Room

TS01 (Sala Aldebaran, Hall 1)

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

ATV GNC for Rendez-vous and docking: Principles, technology and experience

accepted

15'

confirmed

Mr. Olivier Mongrard

European Space Agency (ESA)

The Netherlands

2

Robust controller design methodology for planetary landing system considering 6 degrees of freedom

accepted

15'

confirmed

Mr. Satoshi Ueda

Japan Aerospace Exploration Agency (JAXA)

Japan

3

Relative state vector generation algorithm for on-board navigation for Rendezvous Docking Experiment

accepted

15'

confirmed

Mrs. B.P. Dakshayani

Indian Space Research Organization (ISRO)

India

4

Spacecraft Position and Attitude Maneuvers Using Finite-time Control Technique

accepted

15'

confirmed

Mr. Xiaodong Liu

Tsinghua University

China

5

Distributed Control of Fractionated Spacecraft Based on Cyclic Pursuit Strategies

accepted

15'

no-show

Dr. Min Hu

Academy of Equipment

China

6

Optimization of Sphere Population for Electrostatic Multi Sphere Model

accepted

15'

withdrawn

Mr. Daan Stevenson

Colorado Center for Astrodynamics Research, University of Colorado

United States

7

EXPERIENCE USING AN AUTOMATIC RENDEZVOUS / CAPTURE TEST FACILITY FOR GNC V&V IN A DYNAMIC ENVIRONMENT

accepted

15'

confirmed

Dr. Francisco Caballero

Instituto Nacional de Tecnica Aeroespacial (INTA)

Spain

8

DYNAMIC COORDINATION OF A MULTI-DOF MANIPULATOR-PLATFORM SYSTEM

accepted

15'

confirmed

Dr. Silvio Cocuzza

CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova

Italy

9

Global Low-Thrust Guidance Scheme for Disaggregated Spacecraft Architectures

accepted

15'

confirmed

Prof.Dr. Pini Gurfil

Technion, I.I.T.

Israel

11

Precise Position Control for the Pinpoint Touchdown to the Asteroid Surface

accepted

15'

confirmed

Dr. Yuya Mimasu

Japan Aerospace Exploration Agency (JAXA)

Japan

12

A novel nonlinear control approach for rendezvous and docking maneuvering

accepted

15'

confirmed

Dr. Giuseppe Di Mauro

Politecnico di Milano

Italy

13

Flight Testing of the TriDAR rendezvous and Docking Sensor on the Space Shuttle

accepted

15'

confirmed

Mr. Stephane Ruel

Neptec Design Group

Canada