rootbrowseIAC-22C1session IPIP. Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUMPapers1. Multiple Input Multiple Output Adaptive Controllers for a Titan Rover Concept2. Design and Implementation of a Multi-Mission Torque Model Simulator for Earth Satellites4. Distributed Guidance for Flexible Spacecraft Landing on Asteroid5. A preliminary investigation of aerogravity assist missions to Ceres and other asteroids using various trajectory paths6. Application of singular perturbation theory to space flight dynamics problems7. dynamics in the vicinity of the stable halo orbits8. A variant of the Kármán line theory facilitating the identification of a precise altitude boundary9. A Survey of Longitudinal-Shift Maneuvers Performed by Geosynchronous (GEO) Satellites from 2010 to 202110. Automatic multi-gravity assist trajectory design with modified Tisserand Graphs exploration11. design for earth-mars cycler trajectories based on aero assisted orbital transfer12. On the approximation of gravitational field of a dynamically symmetric rigid body by two balls13. Novel Gear based Actuation Mechanism for Spacecraft’s Attitude Control15. Optimal Control of J2 formations subject to drag using MPC16. machine learning based orbit prediction17. ienai GO: a free tool for concurrent mission design and optimization with on-board electric propulsion18. TudatPy - a versatile open-source astrodynamics software package for space education19. Modelling and simulation of an on-orbit experiment for testing a novel engine technology20. Optimization of chaser trajectory for active debris removal missions22. On optimal three-impulse Earth-Moon transfers in a four-body model24. study of orbital mechanics parameter using Laplace transform.27. Processing of Altimetric Data for Precise Orbit Determination28. Real-time Optimal Control of a 6-DOF State-Constrained Close-Proximity Rendezvous Mission29. A survey of the Magnetic Dipole Moment Determination Methods applied on CubeSats and Nanosatellites30. Singularity-Free Hybrid Control for Autonomous Berthing of Two Spacecrafts31. Initial Guesses for Cislunar Low-Thrust Transfers32. Stabilization of Space-advertisement Satellite Formation34. Low-cost Manufacturing and Testing of Attitude Control Systems for CubeSats35. optimal launch windows for artemis III and beyond leveraging contour maps36. Hybrid Multi-Algorithmic Attitude Determination and Control Architecture37. Families of Displaced non-Keplerian Polar Orbits for Space-Based Solar Energy Applications38. Grid search for spatial axi-symmetric horseshoe orbits in restricted three body problem39. Mapping long-term natural orbits about Titania, a satellite of Uranus42. Data-Driven Guidance for Asteroid Landing Based on Real-Time Dynamic Mode Decomposition43. The thrust vector control optimization of the air-breathing electric propulsion to maintain spacecraft in ultra-low orbits44. Optimization of impulsive low-energy trajectories to the Earth-Moon L2 halo orbit45. physical cross-sectional area modeling of complex structural spacecraft for long-term precision orbit determination46. Optimal Trade-Off between Solar Energy and Control Input while Rendezvous and Docking of a CubeSat with a Rotating Target Spacecraft47. A Framework for Deriving and Validating the Multibody Equations of Motion of Micro-Launchers48. Bald Eagle Search Optimization based Bioinspired Spacecraft Rendezvous- Docking and Space Debris Mitigation49. A Transport Theorem for the Inertia Tensor for Simplified Spacecraft Dynamics Development50. N-Body Problem in Non-Inertial Reference Frame. Application to Full Two-Body Stability Problem51. Accessible and Retrievable Asteroids considering Lunar and Solar Gravity Assists