IP. Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM

Papers

1. Wave-based motion control of flexible space systems

3. Multispectral Image Processing for Navigation Using Low Performance Computing

4. Design of on-board fuel-oxidizer mass estimation algorithm for TeamIndus Lunar landing mission

5. Vision based state estimation using a graph-SLAM approach for proximity operations near an asteroid

6. Fault tolerant attitude control for spacecraft with Lorenz and Magnetic Torques

7. Invariant structures related to long term confinement of captured asteroids in the Earth-Moon system

8. Evaluation of a camera-based pose and shape reconstruction technique for an unknown tumbling target

9. highly accurate guidance algorism for landing on a planet with gravity

10. The Aldrin Cycler Improved by the Lorentz Force

11. GRACE accelerometer calibration by high precision non-gravitational force modelling and its validation

12. Orbit Determination of CE-4’s Relay Satellite in Earth-Moon L2 Libration Point Orbit

13. Control of 6DOF Spacecraft Hovering about Asteroids without Velocity Measurements

14. Relative State Measurement of A Non-Cooperative Spacecraft for Final Approaching Stage of On-Orbit Servicing Using Contour Features

15. Chaotic motions of tethered tug-debris system with fuel residuals

16. autonomous guidance using nonlinear model predictive control for rendezvous and docking with non-cooperative targets

17. Distributed Coordination Control for Multiple Spacecraft with Coupled Attitude and Orbit Dynamics under the Directed Graph

18. dual quaternion based relative navigation for spacecraft proximity operation

19. Inverse-dynamics Particle Swarm Optimization for Real Time Optimal Control: Challenges and Opportunities

20. Space-oriented navigation solutions with integrated sensor-suite: the I3DS H2020 project

21. Investigation into the Controllability of Underactuated Magnetically Stabilized Spacecraft

22. End-of-life disposal design for spacecraft at Libration Points Orbits and an interpretation of their probability of Earth return

23. HIGHER-ORDER CAYLEY TRANSFORM FOR RELATIVE POSE PARAMETERIZATION OF SPACECRAFT

24. Novel orbit improvement method through pseudo relative motion analysis

25. sentinel-3 tandem: from concept to implementation

26. The Borea project: a quadrotor UAV cradle-to-grave design for space GNC prototyping and testing

27. Parameter Determination of Dynamical Systems Using Chaotic Orbits

28. Orbital and Formation Optimization for Space Gravitational Waves Observatory Mission

29. Next steps for the CryoSat-2 mission: Improving sea-ice estimates in joint operations with the ICESat-2 spacecraft.

30. Missions for Asteroid Insertion into Earth-Mars Cycler

31. Mission Design and Analysis for Mars and Phobos Missions via Lunar and Mars-Phobos Distant Retrograde Orbits

32. Fuel-optimal trajectories near Lagrange points

33. Advanced In-Flight Results from the GPS Receiver on SmallGEO

34. advanced approach based on convex programming for mars powered descent guidance

35. Extended reactionless workspace of a space manipulator through reaction wheels

36. The mission's design of a solar sail spacecraft to the nearest circumsolar space, based on a locally-optimal control laws

37. How to Send a Signal to Fixed Ground Antennas from a Non-Geostationary Satellite

38. Proba-3 Mission: In orbit demonstration of a high performance relative position and attitude control

39. Coordinated Capture of a Passive Space Object Using Augmented State Estimation and Neural Networks