session 1

Title

Attitude Dynamics (1)

type

oral

Description

This theme discusses advances in spacecraft attitude dynamics and control, as well as design, testing and performance of novel attitude sensors and actuators. This theme also covers dynamics and control of multiple interconnected rigid and flexible bodies, including tethered systems, and in-orbit assembly.

IPC members

• Co-Chair: Prof. Marcello Romano, Technical University of Munich (TUM), Germany;

• Co-Chair: Prof. Bin Meng, Beijing Institute of Control Engineering, Beijing, 100080, P.R. China, China;

• Rapporteur: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;