session 6

Title: Guidance, Navigation and Control (2)
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: 2014-10-02
Time: 09:45
Room: 801A

IPC members

Co-Chair: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;
Co-Chair: Mrs Benedicte Escudier, Institut Supérieur de l'Aéronautique et de l'Espace (ISAE), France;
Rapporteur: Prof. Fuyuto Terui, Kanagawa Institute of Technology, Japan;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		characteristic model based golden section phase plane adaptive control method and its application in rendezvous and docking	accepted	15'	confirmed	Prof. YongChun Xie	Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)	China
2		PRISMA IRIDES: Close Range Optical Inspection of the non-cooperative Satellite Picard	accepted	15'	withdrawn	Mr. Thomas Karlsson	OHB Sweden	Sweden
3		adaptive finite time control of relative translation in proximity of a freely tumbling spacecraft	accepted	15'	confirmed	Dr. Shunan Wu	Dalian University of Technology (DUT)	China
4		Development of an Integrated Spacecraft Guidance, Navigation, & Control Subsystem for Automated Proximity Operations	accepted	15'	confirmed	Mr. Peter Schulte	School of Aerospace Engineering, Georgia Institute of Technology	United States
5		A testbed for visual based navigation and control during space rendezvous operations	accepted	15'	confirmed	Dr. Marco Sabatini	Sapienza University of Rome	Italy
6		Low-Earth Orbit Spacecraft Relative orbit and attitude decentralized estimation.	accepted	15'	withdrawn	Mr. Adolfo Chaves Jimenez	Delft University of Technology (TU Delft)	The Netherlands
7		Relative Navigation State Estimation Performance for Orbit Debris Removal and Deep-Space Rendezvous	accepted	15'	confirmed	Dr. Jean-Francois Hamel	NGC Aerospace Ltd.	Canada
8		Robust Tether Deployment Control for Electrodynamic Tether Deorbit System	accepted	15'	no-show	Dr. Feng Zhang	China Academy of Launch Vehicle Technology(CALT)	China
9		Towing tethers to control debris removal dynamics	accepted	15'	confirmed	Mr. Riccardo Benvenuto	Politecnico di Milano	Italy
10		Controllability of a Square Solar Sail with Movable Membrane Tips	accepted	15'	confirmed	Mr. Bo Fu		United States
11		analytical three-phase transfer to a solar polar orbit using solar sail propulsion	accepted	15'	confirmed	Ms. Ciara McGrath	University of Strathclyde/Advanced Space Concepts Laboratory	United Kingdom
12		optimal spin rate control of a spinning solar sail for orbital inclination change	accepted	15'	confirmed	Mr. Go Ono	University of Tokyo	Japan
13		A feasibility study of solar radiation pressure feedback control strategy for unstable periodic orbits in the restricted three-body problem	accepted	15'	confirmed	Ms. Stefania Soldini	University of Southampton	United Kingdom