IAF Digital Library

6

session 6

Title: Orbital Dynamics (1)
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.

IPC members

Co-Chair: Mr. Al Cangahuala, National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory, United States;
Co-Chair: Dr. Antonio Prado, National Institute for Space Research - INPE , Brazil;
Rapporteur: Dr. Feng-Tai Hwang, National Space Organization, Taipei;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
2		Leveraging manifolds of tori associated with quasi-satellite orbits to design low-fuel mars-phobos transfers	10	confirmed	Dr. Marc Jorba-Cuscó	Centre National d'Etudes Spatiales (CNES)	France
3		A High-order Target Point Approach to the Stationkeeping of Near Rectilinear Halo Orbits	10	confirmed	Mr. Xiaoyu Fu	Surrey Space Centre, University of Surrey	United Kingdom
4		Cislunar Transfer Design Exploiting Periodic and Quasi-Periodic Orbital Structures in the Four-Body Problem	10	confirmed	Mr. Brian McCarthy	Purdue University	United States
5		Orbital Anomaly Reconstruction Using Deep Symbolic Regression	10	confirmed	Mr. Matteo Manzi	University of Strathclyde	United Kingdom
6		Minimum Cost Relative Dynamics in Cislunar Environment	10	confirmed	Mr. Andrea Capannolo	Politecnico di Milano	Italy
7		Surface Trajectories of Particles on the Primary of the Sphere-Restricted Full 2-Body Problem	10	confirmed	Dr. Yu Jiang	State Key Laboratory of Astronautic Dynamics	China
8		Transfers around Phobos using invariant manifolds of unstable Quasi-Satellite Orbits	10	confirmed	Mr. Nishanth Pushparaj	The Graduate Universty for Advanced Studies[SOKENDAI]	Japan
10		Modelling the break-up and re-entry propagation of meteorites through a continuum approach	10	confirmed	Mr. Simone Limonta	Politecnico di Milano	Italy
11		An analytic method of the density evolution of large constellations and collision probability evaluation	10	confirmed	Ms. Yidan Gao	School of Aerospace Engineering, Beijing Institute of Technology	China
14		Atmosphere impact assessment on the trajectory control problem for a descent module returning from the Moon	10	confirmed	Mr. Marat Airapetyan	Bauman Moscow State Technical University	Russian Federation
15		Complex orbit dynamics of decommissioned geostationary satellites	10	confirmed	Mr. Simone Proietti	Sapienza University of Rome	Italy