IPB. Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM

Papers

1. Deployment of Lunar Orbital Station in High Circular Orbit: Alternative to NRHO

2. General Overview of Near-Earth Magnetic Anomaly Effects on Satellite Attitude Estimation

3. MULTIDUAL QUATERNIONS BASED DYNAMICS MODELING FOR A RIGID-FLEXIBLE COUPLING SPACECRAFT AND APPLICATION

4. A constellation design for orbiting solar reflectors to enhance terrestrial solar energy

5. Boundary-Value Problem of Tisserand-Leveraging Transfers

6. mission to the trans-neptunian object sedna: a possible next step of humanity towards stars

7. The capture of near-Earth asteroids in close proximity orbits with a two-spacecraft strategy using a linear approximation

8. Dynamics and Control of Gyroscopic Stabilized Tether Satellite System in LEO

10. New results on the mass-optimization analysis of a planetary sunshade system

11. study on short range formation flight and docking control using ac magnetic field

12. Distributed Cooperative Spacecraft Surrounding Control with Input Saturation and Collision Avoidance

14. Model Predictive Control with Sequential Convex Programming (SCP) for Cooperative/Non-cooperative Formation Flying Satellites

15. Analysis of the effects of disturbing factors on the dynamics of a spacecraft in low-Earth orbit

17. Convex Optimization of Spacecraft Rest-to-Rest Attitude Reorientation Maneuvers with Keep-Out Constraints

18. attitude and vibration control of a flexible satellite using double-gimbal variable-speed control moment gyro with unbalanced rotor

19. Optimal Steering Law for Single-Gimbal Control Moment Gyroscopes with Singularity Avoidance and Vibration Suppression

20. An Analytical Approach for Constellation Low-Thrust Replenishment Exploiting J2 Effect

21. Observer-based fault-tolerant integrated orbit-attitude control of solar sail

23. Developing an LQR/APF based Orbit correction, Orbit Prediction, and Navigation Control for CubeSat's Formation Flying

24. model predictive control based on recurrent neural network for reusable launch vehicle with dynamics uncertainties

25. Reaction wheels angular momentum management during interplanetary flight

26. Two-impulse orbital transfer based on the solution of Lambert problem with optimal flight time

27. Satellite Characterization Using the Theory of Functional Connections and Nelder-Mead Algorithm

28. Attitude Control of an Earth-pointing Satellite Employing Novel Actuator Configurations for Global Asymptotic Stability

29. Path planning and control for asteroid ejecta collection after a kinetic impact

30. Magnetorquers attitude control for formation flying in LEO

31. Satellite Routing with Quantum Annealing: Collecting Space Debris and On-orbit Servicing

32. Data-driven Online Optimization for Spacecraft Fuel Slosh