session 8
- Title
Attitude Dynamics (1)
- 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.
- Date
2016-09-30
- Time
- Room
- IPC members
Co-Chair: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;
Co-Chair: Prof. Gianmarco Radice, Singapore, Republic of;
Rapporteur: Dr. Shinji Hokamoto, Kyushu University, Japan;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 15' | confirmed | Mr. Dario Spiller | Sapienza University of Rome | Italy | ||
2 | Concept Design for a Satellite with Micro Vibration Isolator | 15' | confirmed | Mr. Takuma Shibata | The Graduate Universty for Advanced Studies[SOKENDAI] | Japan | |
3 | torque distribution algorithm for effective use of reaction wheels torque and angular momentum | 15' | confirmed | Mr. Mikihiro Sugita | Mitsubishi Electric Corporation | Japan | |
4 | Using Aerodynamic Torques to Aid Detumbling into an Aerostable State | 15' | confirmed | Mr. Zhou Hao | The University of Manchester | United Kingdom | |
5 | An attitude determination and control system for a nano-satellite alternative launch platform | 15' | confirmed | Prof. Simone Battistini | Universidade de Brasília | Brazil | |
6 | 15' | confirmed | Mr. XinXin Yu | Beijing Institute of Control Engineering(BICE), China Academy of Space Technology(CAST) | China | ||
7 | Stability Analysis of 3-axis Attitude Control System of Single Wing Satellite | 15' | confirmed | Dr. Hao-Chi Chang | National Space Organization | Taiwan, China | |
8 | Simple Adaptive Control of a Satellite with Large Flexible Appendages | 15' | confirmed | Dr. Derek Gransden | Delft University of Technology (TU Delft) | The Netherlands | |
9 | numerical evaluation of on-orbit attitude behavior for microsatellites with variable shape function | 15' | confirmed | Mr. Kyosuke Tawara | Tokyo Institute of Technology | Japan | |
10 | ACS Feed-Forward for Manipulator Control During Coupled Satellite Detumbling | 15' | withdrawn | Mr. Barrett Dillow | University of Maryland, College Park | United States | |
11 | 15' | confirmed | Prof. Vladimir S. Aslanov | Samara National Research University (Samara University) | Russian Federation | ||
12 | Constraint Force Algorithm for Dynamics Modeling of Flexible Multibody Spacecraft | 15' | confirmed | Ms. LI Haiyan | China | ||
13 | 15' | withdrawn | Dr. Liang Sun | Beihang University | China |