rootbrowseIAC-23C1session IPIP. Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUMPapers1. Dynamic analysis of mechanical motion of a variable-mass rocket system3. Desensitized Ensemble Guidance4. Machine Learning Based Guidance for Optimal Spacecraft De-Orbiting6. Comparison of Non-Linear Heuristic Control and Linear Time-Varying Optimal Control Design for 3-axes Attitude Control of a Microsatellite7. Closed-loop guidance for interplanetary CubeSats with indirect methods8. Robust low-thrust gravity-assist trajectory optimization9. Optimal Tuning of the Nanosatellite Attitude Controller Using TRIAD-Aided Kalman Filter and Particle Swarm Optimization10. THE EXTENDED WAHBA’S PROBLEM IN DUAL AND MULTIDUAL QUATERNIONS11. Approximation for gravitational field of a small celestial body by a triple of uniform balls13. Trajectory Planning and Execution in a Hyper Redundant Continuum Manipulator for Satellite Docking14. Optimal control of the thrust vector of a spacecraft with an air-breathing electric propulsion15. Fuel-Minimum Fuel-Average Control Algorithm for Large Constellation Configuration Maintenance Based on Perturbation Compensation Method16. Minimum-Propellant Direct, Assisted, and Slingshot Return Trajectories from Mars, Jupiter, and their moons17. Attitude determination and control system design for a 3U CubeSat to monitor forward light scattering over Earth horizon20. Three-body Moon-Mars transfer with revisited weak stability boundary concept and aerobraking capture21. Intelligent Integrated Navigation of Solar System Boundary Exploration Cruise Phase Based on Q-Learning Extended Kalman Filter22. Robust Attitude Control Using Electrospray Thruster23. Variable-Performance Electrospray Maneuvers Optimization26. Time-delay flight control of small-scale vertical take-off and vertical landing demonstrator using a mini gas turbine engine27. Design of transfer trajectories from cislunar orbits to the retrograde Geo-Synchronous Orbit