session 5
- Title
Guidance, Navigation & Control (3)
- 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
2022-09-20
- Time
- Room
- IPC members
Co-Chair: Dr. Miguel Bello Mora, Orbex, Spain;
Co-Chair: Prof. Jean de Lafontaine, NGC Aerospace Ltd., Canada;
Rapporteur: Dr. Tang Liang, Beijing Institute of Control Engineering, China Academy of Space Technology (CAST), China;
Rapporteur: Dr. Yung Fu Tsai, Taiwan Space Agency (TASA);
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 15:00 | Risk Guarantees for Integrated Targeting and Guidance during Powered Descent and Landing | 15 | confirmed | Ms. Julia Briden | Massachusetts Institute of Technology (MIT) | United States |
2 | 15:15 | 15 | confirmed | Mrs. Alice De Oliveira | Politecnico di Milano | Italy | |
3 | 15:30 | Real-Time Spacecraft Localization and Mapping with Optical and Radio-Based Artificial Markers | 15 | confirmed | Mr. Genki Ohira | The Graduate Universty for Advanced Studies[SOKENDAI] | Japan |
4 | 15:45 | 15 | Dr. Wenhao Du | CALT,CASC | China | ||
5 | 16:00 | Onboard trajectory optimization for asteroid landing based on General Koopman Operator | 15 | confirmed | Mr. Yang Ni | Northwestern Polytechnical University | China |
6 | 16:15 | Intelligent fuel-optimal guidance strategy for small body flexible landing | 15 | confirmed | Mr. Dongyue Zhao | Beijing Institute of Technology (BIT) | China |
7 | 16:30 | An iterative LQR Method for Addressing Model Uncertainty in the Planetary Entry Problem | 15 | confirmed | Ms. Allegra Farrar | Massachusetts Institute of Technology (MIT) | United States |
8 | 16:45 | Onboard Trajectory Generation for Autonomous Landing on Small Bodies | 15 | withdrawn | Ms. Larissa Balestrero Machado | Universität der Bundeswehr München | Germany |
9 | 17:00 | application of neural ordinary differential equations to trajectory control laws for lunar landing | 15 | confirmed | Mr. Satoshi Ueda | Japan Aerospace Exploration Agency (JAXA) | Japan |
10 | 17:15 | Analysis of Multi-Orbit Multi-Payload Injection Scenarios for an Upper Stage | 15 | confirmed | Mr. Iñigo Alforja Ruiz | Politecnico di Milano | Italy |