session 4
- Title
Guidance, Navigation and Control (2)
- type
oral
- Description
The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft, including formation flying, rendezvous and docking.
- Date
2024-10-18
- Time
- Room
- IPC members
Co-Chair: Dr. Mai Bando, Kyushu University, Japan;
Co-Chair: Prof. Eberhard Gill, Delft University of Technology, The Netherlands;
Rapporteur: Prof. Hanspeter Schaub, Colorado Center for Astrodynamics Research, University of Colorado, United States;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 10:15 | Optimal Guidance Control Considering Multiple Constraints for Asteroid Sample Return | 15 | confirmed | Prof. Toshio Kamiya | Meisei University | Japan |
2 | 10:30 | 15 | confirmed | Mr. Kent Yoshikawa | Japan Aerospace Exploration Agency (JAXA) | Japan | |
3 | 10:45 | On-orbit operation results of the powered descent guidance algorithm for pinpoint lunar landing | 15 | confirmed | Mr. Satoshi Ueda | Japan Aerospace Exploration Agency (JAXA) | Japan |
4 | 11:00 | The Development and Verification Method of SLIM Lunar Landing Navigation Algorithms | 15 | confirmed | Mr. Kentaro Watanabe | Mitsubishi Electric Corporation | Japan |
5 | 11:15 | Integrated Optical Terrain Relative Navigation for Autonomous Lunar Landing | 15 | confirmed | Mr. Giovanni Pio Parracino | Politecnico di Milano | Italy |
6 | 11:30 | 15 | confirmed | Mr. Livio Carzana | Delft University of Technology (TU Delft) | The Netherlands | |
7 | 11:45 | 15 | confirmed | Mr. Nicolo Woodward | Embry-Riddle Aeronautical University | United States | |
8 | 12:00 | Design of Minimum-Time Low-Thrust Transfer between Quasi-Periodic Orbits | 15 | confirmed | Mr. Naoki Hiraiwa | Kyushu University | Japan |
9 | 12:15 | analysis of periodic and quasi-periodic orbits with optimal feedback control | 15 | confirmed | Ms. Ayano Tsuruta | Kyushu University | Japan |
10 | 12:30 | Spacecraft trajectory optimisation using Differential Dynamic Programming | 15 | confirmed | Mr. Pietro Mondino | ISAE - Institut Supérieur de l'Aéronautique et de l'Espace | France |