IAF Digital Library

8

session 8

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: 2018-10-05
Time: 09:45
Room: CCB Borgward

IPC members

Co-Chair: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;
Co-Chair: Dr. Richard Epenoy, Centre National d'Etudes Spatiales (CNES), France;
Rapporteur: Prof. Stéphanie Lizy-Destrez, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;
Rapporteur: Prof. Massimiliano Vasile, University of Strathclyde, United Kingdom;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Current status of the on-going orbit transfer of Super Low Altitude Test Satellite (SLATS)	15	confirmed	Mr. Shunsuke Imamura	Japan Aerospace Exploration Agency (JAXA)	Japan
2		Optimization of Radiation Exposure for Low-thrust Missions with a Shape-based Method	15	confirmed	Dr. Volker Maiwald	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
3		Flower Constellations for Earth Coverage with Big Number of Satellites	15	confirmed	Prof. Yury Razoumny	Peoples' Friendship University of Russia (RUDN University)	Russian Federation
4		Multi-Rendezvous Trajectory Optimization with Neural Network and Reinforcement Learning	15	confirmed	Mr. Haiyang Li	Tsinghua University School of Aerospace	China
5		An Intrusive Polynomial Algebra Multiple Shooting Approach to the Solution of Optimal Control Problems	15	confirmed	Mr. Cristian Greco	University of Strathclyde	United Kingdom
6		Lyapunov-based low-energy low-thrust transfers to the moon	15	confirmed	Dr. Richard Epenoy	Centre National d'Etudes Spatiales (CNES)	France
7		Optimal escape manifolds for cis-lunar Halo orbits	15	confirmed	Mr. Lorenzo Bucci	Politecnico di Milano	Italy
8		Gauss' Variational Equations for low-thrust optimal control problems in low-energy regimes	15	confirmed	Ms. Rita Neves	Cranfield University	United Kingdom
9		Low-Thrust Trajectory Design Via Direct Transcription Leveraging Structures from the Low-Thrust Restricted Problem	15	confirmed	Mr. Robert Pritchett	Purdue University	United States
10		Transfers Between Near-Rectilinear Halo Orbits and the Moon	15	confirmed	Dr. Maksim Shirobokov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
11		On the sophisticated orbit design of the Lunar Meteoroid Impacts Observer CubeSat	15	confirmed	Dr. Diogene Alessandro Dei Tos	Politecnico di Milano	Italy
12		Do You See What I See?: Interactive Visualization of Mission Design and Navigation	15	confirmed	Mr. Jeffrey Stuart	Jet Propulsion Laboratory - California Institute of Technology	United States