session 9
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 and rockets, including formation flying, rendezvous and docking
- Date
2015-10-16
- Time
- Room
- IPC members
Co-Chair: Mrs Benedicte Escudier, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;
Co-Chair: Prof. Arun Misra, Mc Gill Institute for Aerospace Engineering (MIAE), Canada;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | Application of Gauss’ Variational Equations to Relative Orbit Phasing and Acquisition – A Case Study | 16' | withdrawn | Mr. Josh Newman | Space Flight Laboratory, University of Toronto | Canada | |
2 | Optimal Station Keeping by Electric Propulsion in Failure Mode | 16' | confirmed | Mr. Shuge Zhao | Beijing Institute of Technology | China | |
3 | 16' | withdrawn | Dr. Manoranjan Sinha | IIIT Kharagpur | India | ||
4 | 16' | withdrawn | Ms. Ciara McGrath | University of Strathclyde/Advanced Space Concepts Laboratory | United Kingdom | ||
5 | 16' | confirmed | Prof. Adrian-Mihail Stoica | University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space | Romania | ||
6 | Attitude and Position Tracking of a Spacecraft without Velocity Measurement | 16' | withdrawn | Mr. Haichao Gui | York University | Canada | |
7 | Flight Result of the Attitude Determination Using Small Satellite On-board CMOS Camera Image | 16' | no-show | Ms. Chisato Sekigawa | Japan | ||
8 | 16' | no-show | Mr. Dezhen XU | Beijing Institute of Tracking and Telecommunication Technology (BITTT) | China | ||
9 | Coupled orbit-attitude control of a high area-to-mass ratio satellite | 16' | withdrawn | Mr. Yafei Zhao | Harbin Institute of Technology | China | |
10 | Radio Pulsar Navigation Method Based On Synthetic Aperture and Spacecraft Formation Technology | 16' | no-show | Dr. Yu Liu | Shanghai Institute of Spaceflight Control Technology | China | |
11 | adaptive fault-tolerant Coulombic satellite attitude control | 16' | confirmed | Mr. Dipak Kumar Giri | Indian Institute of Technology | India |