IAF Digital Library

9

session 9

Title: Mission Design, Operations and Optimization (2)
Description: This 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: 2010-10-01
Time: 14:00
Room: North Hall

IPC members

Chairman: Prof. Eberhard Gill, Delft University of Technology, The Netherlands;
Chairman: Prof. Michèle Lavagna, Politecnico di Milano, Italy;
Rapporteur: Prof. Kathleen Howell, Purdue University, United States;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Invariant-Manifold, Low-Thrust Transfers to Low Mars Orbits	15	confirmed	Dr. Giorgio Mingotti	University of Strathclyde	United Kingdom
2		Proposed End-of-Mission for the Cassini Spacecraft: Inner D Ring Ballistic Saturn Impact	15	confirmed	Mr. Brent Buffington	National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory	United States
3		Strategy to achieve gravitational capture at Callisto	15	confirmed	Dr. Elisa Maria Alessi	IFAC-CNR	Italy
4		Orbital Transfer Design between Libration Points around Jovian Satellites	15	confirmed	Mr. Keita Tanaka	University of Tokyo	Japan
5		Optimised design of a mission to multiple Trojan asteroids fly-bies	15	confirmed	Mr. denis CARBONNE	Centre National d'Etudes Spatiales (CNES)	France
6		Mission Designs for Solar Probe Plus Enabling Launch Every Year From 2015 Through 2018	15	withdrawn	Dr. Yanping Guo	The John Hopkins University Applied Physics Laboratory	United States
7		finite-thrust optimization of interplanetary transfers of space vehicle with bimodal nuclear thermal propulsion	15	confirmed	Dr. Oleksii Kharytonov	Taras Shevchenko National University	Ukraine
8		Incremental Solution of LTMGA Transfers Transcribed with an Advanced Shaping Approach	15	confirmed	Dr. Massimiliano Vasile	University of Strathclyde	United Kingdom
9		Applications of Multi-Body Dynamical Environments: The ARTEMIS Transfer Trajectory Design	15	confirmed	Mr. David C. Folta	National Aeronautics and Space Administration (NASA), Goddard Space Flight Center	United States
10		Particle Swarm Optimization Applied to Orbital Transfers	15	confirmed	Dr. Mauro Pontani	Sapienza University of Rome	Italy
11		a study of the transfer trajectories to halo orbits using stable manifolds considering launch conditions	15	confirmed	Dr. Masaki Nakamiya	ISAS/JAXA	Japan
12		Deterministic Method for Space Trajectory Design with Mission Margin Constraints	15	confirmed	Dr. Joris Olympio	European Space Agency (ESA)	The Netherlands