IAF Digital Library

5

session 5

Title: Guidance, Navigation and Control (1)
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: 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	Mode	Presentation status	Speaker	Affiliation	Country
1		Orbit determination across unknown maneuvers using the essential thrust Fourier coefficients	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	15'	confirmed	Mr. Matthew Bourassa	Carleton Univeristy	Canada
3		A New Neighboring Optimal Guidance Algorithm for Space Trajectories	15'	confirmed	Dr. Mauro Pontani	Sapienza University of Rome	Italy
4		Onboard navigation for the Canadian Polar Communication and Weather Satellite in Tundra orbit	15'	confirmed	Mr. Warren Soh	Magellan Aerospace	Canada
6		orbital dynamics of formation flying under mass-exchange novel control	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	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	15'	confirmed	Mr. Drew Bittner	West Virginia University	United States
9		Control of Bending/Torsional Vibration of Tape Tether Using Smart Film Sensors/Actuators	15'	confirmed	Prof. Hirohisa Kojima	Tokyo Metropolitan University	Japan
12		design of attitude control system by multi-objective optimization considering practical operation of spacecraft equipped with control moment gyros	15'	confirmed	Ms. Ai Noumi	Keio University	Japan
13		receding-horizon unscented kalman filter for satellite attitude estimation	15'	confirmed	Mr. Ryo Hirasawa	Keio University	Japan