rootbrowseIAC-17C1session IPIP. Interactive PresentationsPapers1. Performance analysis of Fast Unscented Kalman Filters for Attitude Determination in UNSW-EC0 CubeSat Engineering Model2. Analysis of orbits near a binary asteroid system modeled as rotating mass dipoles3. A New Type of Sun Sensor for Micro-Satellite Based on Bionic Compound Eye4. Orbital transfers around a double asteroid system5. Study on the Stability of Nonlinear Time-varying Spacecraft Control System6. Safety Trajectory Optimization in Ultra-close Proximity to Large Debris7. Quaternion based Attitude Stabilization in the Circular Restricted Three-Body Problem8. High Accuracy and High Stability Pointing of Space Telescope Based on Ultra-Quiet Platform9. Late-Life Reconfiguration Maneuvers of the RapidEye Constellation for the Reversal of LTAN Drift10. Planetary UAV exploration simulated in a flying arena with the use of novel dual quaternions attitude dynamics algorithms11. The combined Lambert-Tisserand resolution applied to the single flyby problem12. Goal-oriented planning and path parameterization for time-optimal spacecraft reorientation13. three-channel filter theory for fault detection and isolation of redundant inertial measurement unit14. relative navigation filter algorithm for elliptical orbits based on onboard relative measurements15. A Novel Velocity Observer for 6DOF Spacecraft Formation Flying16. Coordinated Path Planning Strategy for Dual-Arm Space Robot Using B Spline17. Periodic orbits in the Restricted Three-Body Problem with non-spherical mass distribution of primaries18. Delta-V Assisted Homoclinic and Heteroclinic Connections of Periodic Orbits around Natural Equilibrium Points of Irregular Asteroids19. Large-Scale Spacecraft Swarm Decentralized Formation Flying Control Based on Sliding Mode Control and Tracking Differentiator20. safety analysis for near rectilinear orbit close approach rendezvous in the circular restricted three-body problem21. Novel Direct Method for Continuous Thrust Trajectory Optimization22. Software Architecture for Deep-Space Navigation Filter Development23. The Homoclinic and Heteroclinic Connections of Planar Symmetric Resonant Orbits in the Restricted Three-Body Earth-Moon System24. Low-Orbit Spacecraft Service Planning25. AOCS Design and On-orbit Performance of ARASE/ERG Satellite26. Preliminary Study on Vertical Descent Guidance for Precise Lunar Landing27. A Fiber Optic Gyro-Based Attitude Control System for Autonomous Target Tracking28. Using the spacecraft with a solar sail to monitor a specific area of Mars29. Model and trajectory optimization for an ideal laser-enhanced solar sail30. optimization of flyby schemes in the framework of adr mission in leo31. Comparative Assessment of Different Constellation Geometries for Space-based Applications32. Matching of Patched–Integrated Trajectories for Cis-Lunar Transfers33. Searching Reachable Region of Low-Thrust Trajectories by Superposition and Greedy Optimization34. Characterisation of the geopotential deficiencies in SGP4 propagation for drag-less low-earth orbiting test cases35. RELATIVE REACHABLE DOMAIN COMPUTING OF SPACECRAFT WITH SINGLE IMPULSE IN MISSING PERIOD36. The integrated dynamics modeling and coupling analysis for orbit and attitude of spacecrafts