rootbrowseIAC-17C1session 11. Attitude Dynamics (1)Papers1. coulomb tether double-pyramid satellite formations: with application to GEO satellite collocation2. Force and Torque Disturbance Modeling Due to General Thruster Plume Impingements3. Time-Varying Errors for Magnetometers on Small Satellites4. Dynamic Control System Mode Performance of the Space Technology-7 Disturbance Reduction System5. Attitude Stabilization of a Flexible Spacecraft using combined PZT/optical sensors6. magnetic attitude control of satellites using coarse pulse-width-modulation of magnetorquers7. L1 adaptive control of spacecraft flying in very Low Earth Orbits using aerodynamic torques8. Investigation into Integrated Attitude Determination in High-Precision CubeSats9. Multifunctional Optical Attitude Determination Sensor for Picosatellites10. Tether deployment using high spin rate control for interplanetary nanosatellite missions11. Fully-Coupled Dynamical Jitter Modeling of a Rigid Spacecraft with Imbalanced Double-Gimbal Variable-Speed Control Moment Gyros12. High dynamic star tracker for remote sensing satellite