session 4
- Title
Attitude Dynamics (2)
- 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 regidi and flexible bodies, including tethered systems, an in-orbit assembly.
- Date
2014-10-01
- Time
- Room
- IPC members
Co-Chair: Prof.Dr. Kazuya Yoshida, Tohoku University, Japan;
Co-Chair: Dr. Simei Ji, Beijing Institute of Technology, China;
Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | KEYNOTE: Lessons Learned from the Dynamical Behavior of Orbiting Satellites | 30' | confirmed | Dr. Jozef van der Ha | Mission Design & Operations | United States | |
2 | 15' | confirmed | Mr. Jian-Feng Shi | MDA Corporation | Canada | ||
3 | An exponentially fast attitude tracking controller on the rotation group | 15' | confirmed | Dr. James Biggs | University of Strathclyde | United Kingdom | |
4 | active damping algorithm of the international space station structure vibration | 15' | confirmed | Mr. Aleksey Zhirnov | S.P. Korolev Rocket and Space Corporation Energia | Russian Federation | |
5 | A distributed attitude control law for formation flying based on the Cucker-Smale model | 15' | confirmed | Mr. Fabrizio Paita | Universitat Politecnica de Catalunya (UPC) | Spain | |
6 | In Orbit Noise Evaluation of COTS Sensors used for Attitude Determination on AAUSAT3 | 15' | withdrawn | Mr. Michael Nauheimer | Aalborg University | Denmark | |
7 | Retraction of the tether on last stag of the deployment procedure for tether-assisted re-entry | 15' | withdrawn | Prof. Vladimir S. Aslanov | Samara National Research University (Samara University) | Russian Federation | |
8 | Robust Nonlinear Control of Underactuated Spacecraft using a Single Thruster | 15' | confirmed | Mr. Alexander Frias | Ryerson University | Canada | |
9 | 15' | withdrawn | Mr. Albert Caubet | University of Strathclyde | United Kingdom | ||
10 | attitude determination for small spin satellite based on navigation receiver with single antenna | 15' | no-show | Mr. wei wang | Shanghai Institute of Satellite Engineering | China | |
11 | 15' | confirmed | Mr. Ansgar Heidecker | German Aerospace Center (DLR) | Germany | ||
12 | Development of Total Orbital Real-time Attitude control Simulator for Small Satellites | 15' | confirmed | Mr. Takayuki Hosoda | Mitsubishi Precision Co., Ltd. | Japan |