IAF Digital Library

4

session 4

Title: Orbital Dynamics (2)
Description: This theme discusses advances in the knowledge of natural motions of objects in orbit around the Earth, planets, minor bodies, Lagrangian points and more generally natural orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.
Date: 2019-10-23
Time: 09:45
Room: 150A

IPC members

Co-Chair: Prof. Gerard Gomez, University of Barcelona, Spain;
Co-Chair: Prof. Kathleen Howell, Purdue University, United States;
Rapporteur: Dr. Feng-Tai Hwang, National Space Organization, Taipei;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	KEYNOTE: Astrodynamics of Lunar and Cis-Lunar Missions	30	confirmed	Mr. David C. Folta	National Aeronautics and Space Administration (NASA), Goddard Space Flight Center	United States
2	10:15	Manifold-to-manifold transfers using low-thrust acceleration	15	confirmed	Mr. Yuki Kayama	Kyushu University	Japan
3	10:30	Design of Low-Energy Capture trajectories in the Elliptic Restricted Four-Body Problem	15	confirmed	Mr. Stefano Carletta	Sapienza University of Rome	Italy
4	10:45	Sun-Earth libration points transfers through Earth-Moon gravity assist	15	confirmed	Mr. Lorenzo Bucci	Politecnico di Milano	Italy
5	11:00	The Dynamics of Stationkeeping Strategies around Libration Point Orbits	15	confirmed	Dr. Ariadna Farres	NASA Goddard/University of Maryland, Baltimore County (UMBC)	United States
6	11:15	Contributions of Venus Swing-by maneuver in Earth-Mars transfers	15	confirmed	Prof. Maisa Terra	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
7	11:30	Orbit Design and Maintenance in the Elliptical Hill Problem with Applications to the Phobos Sample Return Mission MMX	15	confirmed	Dr. Nicola Baresi	Surrey Space Centre, University of Surrey	United Kingdom
8	11:45	Psyche Mission: Dynamics On and Nearby the Target	15	confirmed	Prof. Othon Winter	UNESP - São Paulo Sate University	Brazil
9	12:00	High-Order Resonant Orbit Manifold Expansions For Mission Design In the Planar Circular Restricted 3-Body Problem	15	confirmed	Mr. Bhanu Kumar	Georgia Institute of Technology	United States
10	12:15	Characterization of low-energy orbits for the exploration of planetary systems	15	confirmed	Dr. Elena Fantino	Khalifa University of Science and Technology (KUST)	United Arab Emirates
11	12:30	Human Agent Planning for Spacecraft Motion subject to Chaotic Dynamics, Small Random Perturbations and Unknown Parameters	15	confirmed	Prof. Davide Guzzetti	Auburn University	United States
*		A new method of refining near-earth object characteristics and behaviours using differential correction.		confirmed	Mr. Richard Samuel	Australian National University (ANU)	Australia