IAF Digital Library

1

session 1

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: 2015-10-12
Time: 15:15
Room: Teddy B (ICC, lower level)

IPC members

Co-Chair: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;
Co-Chair: Mr. Vincent Martinot, Thales Alenia Space France, France;
Rapporteur: Prof. Moriba Jah, Privateer Space, Inc., United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Philae’s Flight Dynamics challenges: report of the landing on a comet	16'	confirmed	Dr. Elisabet Canalias	CNES	France
2		Applicability of the Tisserand Criterion for Optimization of Gravity-Assist Sequences for Low-Thrust Missions	16'	confirmed	Mr. Volker Maiwald	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
3		Survey of Low-Thrust Gravity Assist Trajectory Optimization Methods, with Comparisons to a Novel, Multi-Impulse Discretization Approach	16'	confirmed	Mr. Joshua Fogel	University of Southern California	United States
4		Initial and final boundaries transformation when solving optimal control problem with averaging techniques and application to low thrust orbit transfer	16'	confirmed	Mr. Thierry Dargent	Thales Alenia Space France	France
5		Joint Optimization of the Low-Thrust Trajectory and the Main Design Parameters of Electric Propulsion System	16'	confirmed	Dr. Viacheslav Petukhov	RIAME	Russian Federation
6		low thrust minimum fuel optimization to libration point orbits using variable specific impulse engine	16'	withdrawn	Mr. Hao Zeng	School of Aerospace Engineering, Beijing Institute of Technology	China
7		Optimal Control of Electric Propulsion Spacetag for Operation of the Near Lunar Infrastructure	16'	confirmed	Prof. Olga Starinova	Samara National Research University (Samara University)	Russian Federation
8		Low-thrust trajectory design and operations of PROCYON, the first deep-space micro-spacecraft	16'	confirmed	Dr. Stefano Campagnola	Japan Aerospace Exploration Agency (JAXA)	Japan
9		Optimal 3D Lunar soft landing trajectory design and Performance evaluation of explicit guidance laws	16'	no-show	Mr. Remesh N	Vikram Sarabhai Space Centre (VSSC)	India
10		Asteroid Retrieval Missions Enabled by Invariant Manifold Dynamics	16'	confirmed	Dr. Joan Pau Sanchez Cuartielles	Cranfield University	United Kingdom
11		Trajectory Options for the DART Mission	16'	confirmed	Dr. Justin Atchison	The John Hopkins University Applied Physics Laboratory	United States