session 2
- Title
Attitude Dynamics (2)
- 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.
- Date
2017-09-26
- Time
- Room
- IPC members
Co-Chair: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;
Co-Chair: Prof. Mikhail Ovchinnikov, Keldysh Institute of Applied Mathematics, RAS, Russian Federation;
Rapporteur: Dr. Hao-Chi Chang, tiSPACE Inc., Unknown;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 09:45 | robust collocated sun-pointing control of a large solar power satellite | 15 | withdrawn | Dr. Shunan Wu | Dalian University of Technology (DUT) | China |
2 | 10:00 | Particle Swarm/Differential Evolution Optimizer for Constrained Slew Maneuvers | 15 | confirmed | Prof. Robert G. Melton | Pennsylvania State University | United States |
3 | 10:15 | Usage of solar and gravitational torques for reaction wheels desaturation | 15 | confirmed | Mr. Yaroslav Mashtakov | Keldysh Institute of Applied Mathematics of RAS | Russian Federation |
4 | 10:30 | Kinematic Steering Enabling Speed-Constrained Three-Axes Attitude Control | 15 | confirmed | Prof. Hanspeter Schaub | Colorado Center for Astrodynamics Research, University of Colorado | United States |
5 | 10:45 | Adaptive Spacecraft Attitude Control with Incremental Approximate Dynamic Programming | 15 | confirmed | Ms. Ye Zhou | Delft University of Technology (TU Delft) | The Netherlands |
6 | 11:00 | vision-based attitude determination system for small satellites using unscented kalman filter | 15 | confirmed | Mr. Dagvasumberel Amartuvshin | Kyushu Institute of Technology | Japan |
7 | 11:15 | PID Controller Optimization for Android-Powered Nanosatellites Using Jacobian-Based Scaling | 15 | confirmed | Mr. Mohammad Alsharif | University of Bremen | Germany |
8 | 11:30 | 15 | confirmed | Mr. Aureliano Rivolta | Politecnico di Milano | Italy | |
9 | 11:45 | Spacecraft attitude control system based on Total Energy Control Approach. | 15 | confirmed | Mr. Rolando Cortés | CINVESTAV | Mexico |
10 | 12:00 | A comprehensive study on magnetic actuator design for CubeSat missions. | 15 | confirmed | Ms. Anja Kohfeldt | Technische Universität Berlin | Germany |
11 | 12:15 | Attitude Control of a 3U CubeSat Equipped with a Large Loop Antenna | 15 | confirmed | Ms. Hasnaa Khalifi | University of Florida | United States |
12 | 12:30 | analysis of the attitude motion and structural vibration coupling for solar power satellite | 15 | confirmed | Dr. Shunan Wu | Dalian University of Technology (DUT) | China |