IAF Digital Library

2

session 2

Title: Optimization
Description: Optimization of trajectories including launch, orbital transfer, rendez-vous, atmospheric reentry, manoeuvring and station keeping will be covered in this session.
Date: 2008-09-30
Time: 10:00
Room: Argyll 1

IPC members

Chairman: Mr. David C. Folta, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;
Chairman: Prof. Mauricio Moshe Guelman, Asher Space Research Institute, Technion, I.I.T., Israel;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		concurrent optimization of launcher architectures and ascent trajectories with global optimization algorithms	presentation		Mr. Francesco Castellini	Politecnico di Milano	Italy
2		The Semantic Asteroids	presentation		Dr. Dario Izzo	European Space Agency (ESA)	The Netherlands
3		Design Space Pruning Heuristics and Global Optimization Method for Conceptual Design of Low-Thrust Asteroid Tour Missions	presentation		Ms. Kristina Alemany	School of Aerospace Engineering, Georgia Institute of Technology	United States
4		Method for Optimization of Trajectories Including Gravitational Maneuvers of a Spacecraft with a Solar Sail	presentation		Mr. Pavel Kazmerchuk	Lavochkin Association	Russian Federation
5		A Fast Second-Order Algorithm for Preliminary Design of Low-Thrust Trajectories	presentation		Dr. Gregory Lantoine	Jet Propulsion Laboratory	United States
6		MDO approach for early design of aerobraking orbital transfer vehicles	presentation		Mr. Nicolas Bérend	Office National d’Etudes et de Recherches Aérospatiales (ONERA)	France
7		optimal maneuver strategy and orbit design for servicing spacecraft	presentation		Dr. Xiaohong Yu	Beijing University of Aeronautics and Astronautics (BUAA)	China
8		Optimization of Low-Thrust Many-Revolution Transfers and Lyapunov-Based Guidance	presentation		Dr. Yang Gao	Academy of Opto-Electronics, Chinese Academy of Sciences	China
9		Orbit Synthesis for Hayabusa-2 and Marco Polo (Hayabusa mk-II) Primitive Bodies Sample & Return Missions	presentation		Dr. Junichiro Kawaguchi	Japan Aerospace Exploration Agency (JAXA)	Japan
10		Comparative study on the application of evolutionary optimisation techniques to orbit transfer manoeuvres	discussion		Dr. Giulio Avanzini	Università del Salento	Italy
11		Interactive Optimization Approach for Optimal Impulsive Rendezvous Using Primer Vector and Evolutionary Algorithms	discussion		Dr. Ya-Zhong Luo	National University of Defense Technology	China