IAF Digital Library

1

session 1

Title: Mission Design, Operations & Optimization (1)
type: oral
Description: The theme covers design, operations and optimization of Earth-orbiting and interplanetary missions, with emphasis on studies and experiences related to current and future missions.
Date: 2019-10-21
Time: 15:00
Room: 150A

IPC members

Co-Chair: Prof. Massimiliano Vasile, University of Strathclyde, United Kingdom;
Co-Chair: Mr. Vincent Martinot, Thales Alenia Space France, France;
Rapporteur: Dr. Richard Epenoy, Centre National d'Etudes Spatiales (CNES), France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:00	Riemannian optimization for spacecraft trajectory design	15	confirmed	Mr. Kyosuke Asaki	Kyushu University	Japan
2	15:15	Low-thrust Trajectory Optimisation through Differential Dynamic Programming Method based on Keplerian Orbital Elements	15	confirmed	Mr. Marco Nugnes	Politecnico di Milano	Italy
3	15:30	Concepts and Applications of Aerodynamic Attitude and Orbital Control for Spacecraft in Very Low Earth Orbit	15	confirmed	Ms. Sabrina Livadiotti	The University of Manchester	United Kingdom
4	15:45	FLEX tandem with Sentinel-3	15	confirmed	Mrs. Itziar Barat	ESA - European Space Agency	The Netherlands
5	16:00	New Earth Observation Multi-Satellite Mission Concepts and Space Architectures for Disaster Risk Reduction	15	confirmed	Ms. Stefania Cornara	Deimos Space S.L.	Spain
6	16:15	optimization of transfer schemes between passive space objects in geo vicinity	15	confirmed	Dr. Andrey Baranov	Keldysh Institute of Applied Mathematics of RAS	Russian Federation
7	16:30	constraint analysis for servicing co-located satellites	15	confirmed	Mr. Manwei Chan	Massachusetts Institute of Technology (MIT)	United States
8	16:45	Trajectory Optimization Using Mixed Minimum-Error and Minimum-Fuel Cost Functions	15	confirmed	Ms. Erica Jenson	University of Colorado Boulder	United States
9	17:00	Trajectory optimization in the Three-body problem for a lunar transportation system	15	confirmed	Mr. Mauro Viturro Balufo	SUPAERO- Ecole Nationale Supérieure de l'Aéronautique et de l'Espace	France
10	17:15	Low-Thrust Trajectory Design for a Cislunar CubeSat Leveraging Structures from the Bicircular Restricted Four-Body Problem	15	confirmed	Mr. Robert Pritchett	Purdue University	United States
11	17:30	Mission Design for Close-range Lunar Mapping by Quasi-Frozen Orbits	15	confirmed	Mr. Sandeep Singh	Texas A&M University	United States
12	17:45	Formation Reconfiguration and Science Planning Architecture for the IRASSI Space Interferometer	15	confirmed	Ms. Luisa Buinhas	Bundeswehr University Munich	Germany
*		Orbital insertion around Phobos via ballistic capture and its application to the Martian Moons eXploration mission		withdrawn	Dr. Diogene Alessandro Dei Tos	Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)	Japan