IAF Digital Library

8

session 8

Title: Orbital Dynamics (1)
type: oral
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: 2025-10-02
Time: 10:15
Room: Room C4.8

IPC members

Co-Chair: Dr. Yuichi Tsuda, Japan Aerospace Exploration Agency (JAXA), Japan;
Co-Chair: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;
Rapporteur: Prof. Kathleen Howell, Purdue University, United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Transitioning Quasi-Periodic Orbits to a Full Ephemeris Model	15		Mr. Guido Grossi	Politecnico di Milano	Italy
2	10:30	Transitioning Periodic Orbits in Cislunar Space from Lower to Higher Fidelity Dynamics Representations	15		Mr. Robert Bennett	The University of Texas at Austin	United States
3	10:45	Constructing High-Fidelity Spacecraft Trajectory Baselines with Higher-Dimensional Invariant Tori	15		Dr. Gavin Brown	University of Colorado Boulder	United States
4	11:00	Tesseral effects on the design of low-lunar orbits	15		Dr. Martin Lara	Universidad de La Rioja	Spain
5	11:15	mission design using resonant terminator orbits around a small body	15		Mr. Tomohiro Ishizuka	ISAE-Supaero University of Toulouse	France
6	11:30	Periodic Distant Spherical Orbit with Various Inclinations in Cislunar Space for Station-Keeping	15		Mr. Junji Kikuchi	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
7	11:45	Semi-analytical methods in orbital dynamics: leveraging computational advances for improved dynamical analysis	15		Mr. Ruilong Li	Northwestern Polytechnical University	China
8	12:00	On the Sun-driven long-lasting temporary capture\\ in the Earth-Moon system	15		Dr. Elisa Maria Alessi	Consiglio Nazionale delle Ricerche (CNR)	Italy
9	12:15	Semi-analytical estimation of the probability of capture into 2:3 ground-track resonance of Dawn around Vesta.	15		Mr. Wail Boumchita	University of Strathclyde	United Kingdom
10	12:30	Analysis and Design of Ballistic Escape Trajectories in the Sun-Perturbed Earth-Moon System	15		Mr. Shuya Sano	Kyushu University	Japan
1*	10:15	Atmospheric density estimation from accelerometer data and non-gravitational force modeling applied to replace GRACE-FO's broken accelerometer in gravity field determination.	15		Dr. Benny Rievers	ZARM, University of Bremen	Germany
2*	10:30	a direct solution to the j2 perturbed lambert's problem	15		Mr. Kellen Martin	Iowa State University	United States