session 5

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: 2014-10-01
Time: 14:45
Room: 801A

IPC members

Co-Chair: Prof. Eberhard Gill, Delft University of Technology, The Netherlands;
Co-Chair: Dr. James O'Donnell, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;
Rapporteur: Prof. Igor V. Belokonov, Samara National Research University (Samara University), Russian Federation;

papers
Order	Time	Paper title	Selection result	Mode	Presentation status	Speaker	Affiliation	Country
1		Orbit determination across unknown maneuvers using the essential thrust Fourier coefficients	accepted	15'	confirmed	Mr. Hyun Chul Ko	Colorado Center for Astrodynamics Research, University of Colorado	United States
2		Exploiting Lunisolar Perturbations Using the Grazing Method: An Orbit Control Strategy for a Satellite in a Critically-Inclined Highly Eccentric Orbit Around the Earth	accepted	15'	confirmed	Mr. Matthew Bourassa	Carleton Univeristy	Canada
3		A New Neighboring Optimal Guidance Algorithm for Space Trajectories	accepted	15'	confirmed	Dr. Mauro Pontani	Sapienza University of Rome	Italy
4		Onboard navigation for the Canadian Polar Communication and Weather Satellite in Tundra orbit	accepted	15'	confirmed	Mr. Warren Soh	Magellan Aerospace	Canada
5		Autonomous Collocation of Geosynchronous Satellites	accepted	15'	withdrawn	Prof. Mauricio Moshe Guelman	Asher Space Research Institute, Technion, I.I.T.	Israel
6		orbital dynamics of formation flying under mass-exchange novel control	accepted	15'	confirmed	Dr. Danil Ivanov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
7		State estimation for spacecraft formation flying based on the separation principle	accepted	15'	confirmed	Mr. Leonel Palacios	University of Glasgow	United Kingdom
8		Development of an Alignment Technique for a Large Number of Redundant Inertial Measurement Units	accepted	15'	confirmed	Mr. Drew Bittner	West Virginia University	United States
9		Control of Bending/Torsional Vibration of Tape Tether Using Smart Film Sensors/Actuators	accepted	15'	confirmed	Prof. Hirohisa Kojima	Tokyo Metropolitan University	Japan
10		Robust Constrained Nonlinear Feedback Control for Spacecraft Trajectory Maneuver with Coupled Orbit and Attitude Motion under Multiple Fuel Slosh Modes	accepted	15'	withdrawn	Mr. Insu Chang	University of Illinois at Urbana-Champaign	United States
11		Utilization of video navigation for attitude determination of Soyuz rocket upper stage after payload separation	accepted	15'	withdrawn	Prof. Igor V. Belokonov	Samara National Research University (Samara University)	Russian Federation
12		design of attitude control system by multi-objective optimization considering practical operation of spacecraft equipped with control moment gyros	accepted	15'	confirmed	Ms. Ai Noumi	Keio University	Japan
13		receding-horizon unscented kalman filter for satellite attitude estimation	accepted	15'	confirmed	Mr. Ryo Hirasawa	Keio University	Japan