session 9

1

Single sensor spacecraft can now become reality with HYDRA qualification

15'

Mr. Ludovic Blarre

SODERN

France

2

initial checkout results of the attitude and orbit control subsystem of greenhouse gases observing satellite (GOSAT)

15'

Mr. Keita Sawayama

Mitsubishi Electric Corporation

Japan

3

Measurement of the solar array panel’s vibration caused by thermal snap and delta-V using monitor cameras on the Greenhouse gases Observing Satellite (GOSAT)

15'

Prof.Dr. Mitsushige Oda

Japan Aerospace Exploration Agency (JAXA)

Japan

4

Preliminary Analysis on Attitude Determination Accuracy for Next-generation Korean Multi-Purpose Geostationary Satellite

15'

Dr. Gwanghyeok Ju

Korea Aerospace Research Institute (KARI)

Korea, Republic of

5

On-Orbit Calibration of Precision Star Tracker for the Advanced Land Observing Satellite (ALOS)

15'

Dr. Takanori Iwata

Japan Aerospace Exploration Agency (JAXA)

Japan

8

New methods for accurate thermal disturbance force calculation with application to Pioneer and Flyby anomaly

15'

Dr. Benny Rievers

ZARM University of Bremen

Germany

9

Solar Radiation Pressure Model for Attitude Motion of Hayabusa in Return Cruising

15'

Dr. Yuya Mimasu

Japan Aerospace Exploration Agency (JAXA)

Japan

10

Attitude Control of "Hayabusa" Using Only Ion Thrusters for the Case of RWs Anomaly

15'

Mr. Shogo Sato

The University of TOKYO, Graduate school

Japan