rootbrowseIAC-22C1session 11. Attitude Dynamics (1)Papers1. Design, realization and characterization of a free-floating platform for flexible satellite control experiments2. Reinforcement Learning for Attitude Control of a Spacecraft with Flexible Appendages3. reaction wheel unloading using external torque for variable shape spacecraft4. Fuzzy-Logic-Based Integrated Orbit-Attitude-Vibration Prescribed-Time Control for Large-Scale Flexible Spacecraft5. Online policy iteration ADP-based control of post-capture combined spacecraft without inertia identifications6. Attitude control of satellites with flexible appendages using inverse simulation7. Time-Optimal Attitude Controller Design for Precision Pointing of an Agile Spacecraft using Deep Reinforcement Learning8. Invariant Sigma-Point Kalman Filtering on SO(3) for Attitude Estimation of a 3U CubeSat9. Simultaneous Orbit-Attitude Control of Formation Flying Solar Sails around Sun-Earth L2 Using Reflectivity Modulation10. Attitude Determination and Control System of the Student Small Satellite (SSS): An International Hands-On Satellite Project Among Asia Pacific Universities