rootbrowseIAC-05C1session 33. Attitude Control, Sensors and ActuatorsPapers1. Attitude Control of Vehicle Ikar at Orbiting and Placement of Globalstar Satellites 2. Attitude control of satellites in earth and moon orbits4. Synthesis of optimal control strategy by damping a vibration of Earth satellite with a gravity-gradient stabilization with incomplete information about the state5. Design for robustness using the mu-synthesis applied to Launcher Attitude and Vibration Control6. Advanced Attitude Control of Pico Sized Satellites7. Spacecraft Optical Beam Jitter Control8. Optimal Torque Assignment for Redundant Wheels9. Non-linear Dynamic Inversion versus Gain Scheduling Techniques for Re-entry Flight Control System10. Tethered Interferometric Constellations with Self-Stabilizing Platforms’ Attitude Control