session 3

Title: Guidance, Navigation and Control (1)
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: 2013-09-24
Time: 14:45
Room: 306A

IPC members

Chairman: Prof. Fuyuto Terui, Kanagawa Institute of Technology, Japan;
Chairman: Dr. Bernard Lübke-Ossenbeck, OHB System AG-Bremen, Germany;
Rapporteur: Prof. Paolo Teofilatto, Sapienza University of Rome, Italy;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Guidance, Navigation, and Control System Performance During the Landsat Data Continuity Mission Launch and Commissioning	accepted	15'	withdrawn	Dr. James O'Donnell	National Aeronautics and Space Administration (NASA), Goddard Space Flight Center	United States
2		Phase space and orbit relative motion between high area-to-mass ratio spacecraft	accepted	15'	withdrawn	Dr. Camilla Colombo	University of Southampton	Italy
3		A Linear Constant Gain Controller based on Integrated Guidance and Control for the re-entry phase of a manned space mission	accepted	15'	confirmed	Mr. Pitchaimani M	ISTRAC/ISRO	India
4		Innovative Mars EDL GNC technologies for future China Mars exploration	accepted	15'	confirmed	Prof. Shuang Li	Nanjing University of Aeronautics and Astronautics	China
5		Inter-satellite Orientation Observation and Long-term Autonomous Orbit Determination for Constellation	accepted	15'	confirmed	Mr. Fei Han	Shanghai Key Laboratory of Aerospace Intelligent Control Technology	China
6		A Mixed Kalman/H-infinity Filtering Approach for Augmented Proportional Navigation Guidance	accepted	15'	confirmed	Prof. Adrian-Mihail Stoica	University POLITEHNICA of Bucharest - Research Center for Aeronautics and Space	Romania
7		Attitude Control of Spacecraft using Optimal Nonlinear Control SDRE and Theta-D	accepted	15'	confirmed	Prof. M. Navabi		Iran
8		application of plural momentum exchange impact dampers to landing gear systems	accepted	15'	confirmed	Mr. Tsubasa Watanabe	Nagoya University	Japan
9		Optimal guidance for soft landing on irregular-shaped asteroids using sliding-mode control	accepted	15'	confirmed	Mr. Hongwei YANG	Tsinghua University	China
10		On the Cucker-Smale flocking model applied to a formation moving in a central force-field	accepted	15'	confirmed	Mr. Fabrizio Paita	Universitat Politecnica de Catalunya (UPC)	Spain
11		An Exploration of Numerical Methods for Low-Thrust Trajectory Optimization in N-Body Models	accepted	15'	confirmed	Prof. Franco Bernelli-Zazzera	Politecnico di Milano	Italy
12		Visual Navigation Performance for precise Lunar Landing: Status of a Technological Breakthrough	accepted	15'	withdrawn	Mr. Giovanni Orlando	EADS Astrium Space Transportation GmbH	Germany
13		The Shenzhou Manned Spacecraft Rendezvous and Docking Guidance, Navigation and Control Design	accepted	15'	confirmed	Prof.Dr. Hu Jun	Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)	China