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  • IP. Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM

    Papers

    1. Dynamic analysis of mechanical motion of a variable-mass rocket system

    3. Desensitized Ensemble Guidance

    4. Machine Learning Based Guidance for Optimal Spacecraft De-Orbiting

    6. Comparison of Non-Linear Heuristic Control and Linear Time-Varying Optimal Control Design for 3-axes Attitude Control of a Microsatellite

    7. Closed-loop guidance for interplanetary CubeSats with indirect methods

    8. Robust low-thrust gravity-assist trajectory optimization

    9. Optimal Tuning of the Nanosatellite Attitude Controller Using TRIAD-Aided Kalman Filter and Particle Swarm Optimization

    10. THE EXTENDED WAHBA’S PROBLEM IN DUAL AND MULTIDUAL QUATERNIONS

    11. Approximation for gravitational field of a small celestial body by a triple of uniform balls

    13. Trajectory Planning and Execution in a Hyper Redundant Continuum Manipulator for Satellite Docking

    14. Optimal control of the thrust vector of a spacecraft with an air-breathing electric propulsion

    15. Fuel-Minimum Fuel-Average Control Algorithm for Large Constellation Configuration Maintenance Based on Perturbation Compensation Method

    16. Minimum-Propellant Direct, Assisted, and Slingshot Return Trajectories from Mars, Jupiter, and their moons

    17. Attitude determination and control system design for a 3U CubeSat to monitor forward light scattering over Earth horizon

    20. Three-body Moon-Mars transfer with revisited weak stability boundary concept and aerobraking capture

    21. Intelligent Integrated Navigation of Solar System Boundary Exploration Cruise Phase Based on Q-Learning Extended Kalman Filter

    22. Robust Attitude Control Using Electrospray Thruster

    23. Variable-Performance Electrospray Maneuvers Optimization

    26. Time-delay flight control of small-scale vertical take-off and vertical landing demonstrator using a mini gas turbine engine

    27. Design of transfer trajectories from cislunar orbits to the retrograde Geo-Synchronous Orbit