IAF Digital Library

2

session 2

Title: Guidance, Navigation & 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: 2016-09-27
Time: 09:45
Room: Salon Jalisco E6

IPC members

Co-Chair: Dr. Shoji Yoshikawa, Mitsubishi Electric Corporation, Japan;
Co-Chair: Prof. Moriba Jah, Privateer Space, Inc., United States;
Rapporteur: Dr. Stephan Theil, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Mapping asteroid surfaces with rover swarms	15'	confirmed	Mr. William Crowe	UNSW Australia	Australia
2		HIL testing of a vision-based autonomous GNC for the AIM mission	15'	confirmed	Mr. Andrea Pellacani	G.M.V. Space and Defence, S.A.	Spain
3		Embedded Model Control GNC for the Next Generation Gravity Mission	15'	confirmed	Mr. Luigi Colangelo	Politecnico di Torino	Italy
4		Development of a Combined Attitude and Position Controller for a Satellite Simulator	15'	confirmed	Mr. Marco Sagliano	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
5		Integrated 6-DOF spacecraft orbit-attitude dynamics modeling and its application in hovering control over an asteroid	15'	withdrawn	Dr. Yue Wang	Beihang University	China
6		Far range formation Flight with high risk debris in Low Earth Orbit using relative orbital elements	15'	confirmed	Mr. Mohamed Khalil Ben Larbi	Technische Universität Braunschweig, Institute of Aerospace Systems	Germany
7		Autonomous Navigation and Guidance for Terminal Maneuver For Docking Using Model Predictive Static Programming (MPSP) and Unscented Kalman Filter (UKF)	15'	confirmed	Mr. RaviKumar L	ISRO Satellite Centre (ISAC)	India
8		Fractionated Satellite Systems: Station Keeping Strategies	15'	confirmed	Mr. Daniele Filippetto	Politecnico di Milano	Italy
9		Bounded motions near equilibrium points of contact binary asteroids by a Hamiltonian structure-preserving controller and its applications	15'	confirmed	Dr. Yuying Liang		China
10		Rate Estimation and Damping of a Highly Asymmetrical Tumbling Spacecraft Using Magnetometer Data	15'	confirmed	Ms. shubha kapoor	Indian Space Research Organization (ISRO)	India
11		reaction-wheels based aocs for high-pointing accuracy and stability	15'	confirmed	Ms. Francesca Cirillo	Airbus Defence & Space	Germany
12		Magnetometer Only Attitude Estimation for Spin Satellites	15'	withdrawn	Dr. Halil Ersin Soken	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan