IAF Digital Library

6

session 6

Title: Mission Design, Operations & Optimization (1)
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: 2017-09-28
Time: 09:45
Room: Hall A

IPC members

Co-Chair: Prof. Michèle Lavagna, Politecnico di Milano, Italy;
Co-Chair: Prof. Stéphanie Lizy-Destrez, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;
Rapporteur: Mr. Vincent Martinot, Thales Alenia Space France, France;
Rapporteur: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Novel Piecewise Trajectory Shaping in Hill's Canonical Variables	15	confirmed	Mr. Cristian Greco	Delft University of Technology (TU Delft)	The Netherlands
2		Indirect optimization of low-thrust Earth-Moon transfers in the Sun-Earth-Moon system	15	confirmed	Dr. Richard Epenoy	Centre National d'Etudes Spatiales (CNES)	France
3		Costate Scaling for Multi-Rendezvous Low-Thrust Trajectory Optimization	15	confirmed	Mr. Shiyu Chen	Tsinghua University School of Aerospace	China
4		IRASSI InfraRed Space Interferometer: Mission Analysis, Spacecraft Design and Formation Flying Overview	15	confirmed	Ms. Luisa Buinhas	Bundeswehr University Munich	Germany
5		N-body boundary value problem solver using monotonic basin hopping with applications to Earth-Moon transfer	15	confirmed	Mr. Weichen Xiao	The Hong Kong University of Science and Technology	China
6		Time-optimal solar sail heteroclinic connections for an Earth-Mars cycler	15	confirmed	Ms. Merel Vergaaij	Delft University of Technology (TU Delft)	The Netherlands
7		Flower Constellations in Locally Geostationary Orbits for Earth Regional Coverage	15	withdrawn	Prof. Yury Razoumny	RUDN University	Russian Federation
8		Approximation by filtering in optimal control and applications to low thrust orbit transfer	15	confirmed	Mr. Thierry Dargent	Thales Alenia Space France	France
9		Optimisation tool for low thrust orbit raising based on the Sequential Gradient Restoration Algorithm	15	confirmed	Dr. Francesca Letizia	OHB System AG-Bremen	Germany
10		Optimization of low thrust orbital transfer using the evolution strategies with covariance matrix adaptation	15	withdrawn	Dr. Min Thein	Moscow Aviation Institute (National Technical University, MAI)	Russian Federation
11		THE OPTIMAL TRAJECTORY FOR OBSERVING NON-COOPERATIVE TARGET WITH KOZs CONSTRAINTS	15	confirmed	Mr. Junhua Zhang	National Key Laboratory of Aerospace Flight Dynamic, Northwestern Polytechnical University	China
12		In-Flight Results from the GPS Receiver on SmallGEO	15	confirmed	Dr. Bernard Lübke-Ossenbeck	OHB System AG-Bremen	Germany