session 1
Mission Design, Operations and Optimization - Part 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
2011-10-03
- Time
- Room
- IPC members
Chairman: Mr. Nicolas Bérend, ONERA - The French Aerospace Lab, France;
Chairman: Prof. Yury Razoumny, RUDN University, Russian Federation;
Rapporteur: Mr. Johannes Schoenmaekers, European Space Operations Centre, Germany;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | Trajectory Tour of the Trojan Asteroids Generated via an Optimal Low-Thrust Algorithm | 15 | confirmed | Mr. Jeffrey Stuart | Purdue University | United States | |
2 | Optimum design of power-limited propulsion systems with application to fast Earth-to-Mars transfer | 15 | confirmed | Mr. Nicolas Bérend | Office National d’Etudes et de Recherches Aérospatiales (ONERA) | France | |
3 | A study of the Accessibility to Asteroids for IKAROS Mission after Venus Flyby | 15 | confirmed | Dr. masaki nakamiya | Kyoto University | Japan | |
4 | 15 | confirmed | Mr. Tim Nikolayzik | University of Bremen | Germany | ||
5 | Fuel-Optimal Low-Thrust Trajectory Optimization of Multiple Asteroid Exploration Missions | 15 | no-show | Dr. Yang Chen | Tsinghua University | China | |
6 | Trajectory Optimization of Air-launched rockets via Direct Collocation Method | 15 | withdrawn | Dr. Mauro Pontani | Sapienza University of Rome | Italy | |
7 | Mission Analysis of Robotic, Low-Thrust Missions to the Martian Moons Deimos and Phobos | 15 | confirmed | Mr. Uwe Derz | EADS Astrium Space Transportation GmbH | Germany | |
8 | Trajectory Design in Proximity of Mars for Round-Trip Missions | 15 | withdrawn | Mr. Cyrus Foster | NASA Ames Research Center | United States | |
9 | Mission Design and Analysis for a Laser Occultation Demonstration Mission | 15 | confirmed | Mr. Matthias Renard | Deimos Space S.L. | Spain | |
10 | Continuous Low-Thrust Trajectory Optimization Based on a Symplectic Conservative Perturbation Method | 15 | no-show | Dr. liu luhua | National University of Defense Technology | China | |
11 | Design of optimal Earth pole-sitter transfers using low-thrust propulsion | 15 | confirmed | Dr. Jeannette Heiligers | University of Strathclyde | United Kingdom | |
12 | 15 | confirmed | Dr. Francesco Topputo | Politecnico di Milano | Italy |