session 4

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 formation flying, rendezvous and docking.

Date

2013-09-25

Time

09:45

Room

306A

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Method of Virtual Trajectories for the Preliminary Design of Multiple Gravity-Assist Interplanetary Trajectories

accepted

15'

confirmed

Mr. Sergey Trofimov

Keldysh Institute of Applied Mathematics, RAS

Russian Federation

2

Unobserved maneuver reconstruction and propagation using the Essential Thrust Fourier Coefficients

accepted

15'

confirmed

Mr. Hyun Chul Ko

Colorado Center for Astrodynamics Research, University of Colorado

United States

3

Orbit control of asteroids in libration point orbits for resource exploitation

accepted

15'

confirmed

Dr. Matteo Ceriotti

University of Glasgow

United Kingdom

4

Precise Point Positioning of Megha-Tropiques using ROSA Data

accepted

15'

confirmed

Dr. Narayanasetti Venkata Vighnesam

Indian Space Research Organization (ISRO)

India

5

Precise Spin Sync Slew Control based on Nonlinear Optimization for Spinning Spacecraft

accepted

15'

confirmed

Dr. Yunhua Wu

Nanjing University of Aeronautics and Astronautics

China

6

SINPLEX: A SMALL INTEGRATED NAVIGATION SYSTEM FOR PLANETARY EXPLORATION

accepted

15'

confirmed

Mr. Erik Laan

TNO

The Netherlands

7

Disturbance Torque Estimation and Compensation Scheme for Three-Axis Attitude Control of Spacecraft using Magnetic Torquers

accepted

15'

confirmed

Mrs. KanuPriya Govila

ISRO Satellite Centre (ISAC)

India

8

Design Nonlinear Model Predictive Controller for Space Redundant Manipulators

accepted

15'

confirmed

Mr. Mingming Wang

Technical University of Munich

Germany

9

Singular Steering Logic Analysis using Control Moment Gyros for Nano-Satellite TSUBAME

accepted

15'

confirmed

Ms. Ting Hao

Tokyo Institute of Technology

Japan

10

Optimal-Sliding-Mode-Based Relative Position and Attitude Coupled Control for Autonomous Rendezvous and Docking to a Tumbling Target

accepted

15'

confirmed

Dr. Wei LU

Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

China

11

Autonomous GNC for asteroid deflection and attitude control via laser ablation

accepted

15'

confirmed

Mr. Massimo Vetrisano

University of Strathclyde

United Kingdom

12

Attitude Maneuver Control of a Spacecraft by One Variable-Speed Control Moment Gyros

accepted

15'

confirmed

Mr. Haichao Gui

Beihang University

Canada

13

Adaptive semi-analytical guidance for autonomous planetary landing

accepted

15'

confirmed

Mr. Paolo Lunghi

Politecnico di Milano

Italy