IAF Digital Library

3

session 3

Title: Guidance, Navigation & 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: 2017-09-26
Time: 14:45
Room: Hall A

IPC members

Co-Chair: Prof. Yong Chun Xie, Beijing Institute of Control Engineering, China Academy of Space Technology (CAST), China;
Rapporteur: Prof. Fuyuto Terui, Kanagawa Institute of Technology, Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1		Semi-autonomous attitude guidance using relative navigation based on Line of Sight measurements – AIM scenario	15	confirmed	Mr. Andrea Pellacani	G.M.V. Space and Defence, S.A.	Spain
2		Toward Autonomous Relative Navigation Using Flash LIDAR	15	withdrawn	Prof. Jay McMahon	Colorado Center for Astrodynamics Research, University of Colorado	United States
3		Monocular vision based simultaneous localization and mapping for close proximity navigation near an asteroid	15	confirmed	Mr. Arunkumar Rathinam	University of New South Wales	Australia
4		Accurate penetrator for the in-situ astrobiological exploration of Europa	15	confirmed	Mr. Konstantinos Konstantinidis	Universität der Bundeswehr München	Germany
5		Monocular and LIDAR based determination of shape, relative attitude and position of a non-cooperative, unknown satellite	15	confirmed	Mr. Renato Volpe	University of Rome "La Sapienza"	Italy
6		On the usage of multi-beam laser altimetry for small-body exploration	15	withdrawn	Ms. Graciela González Peytaví	Universität der Bundeswehr München	Germany
7		vision-based state estimation of an uncooperative space object	15	confirmed	Mr. Vincenzo Pesce	Politecnico di Milano	Italy
8		a robust path-tracking guidance considering uncertainty for mars atmospheric entry	15	confirmed	Dr. Zhengshi Yu	School of Aerospace Engineering, Beijing Institute of Technology	China
9		Development and Validation of GNC Functional Modes for Asteroids Sample Return Mission in the frame of the European Commission H2020 NEOShield-2 Project	15	confirmed	Mr. Matteo Suatoni	G.M.V. Space and Defence, S.A.	Spain
10		Spacecraft Navigation Using Gravity Gradient Invariants Based on Cubature Kalman Filter	15	withdrawn	Dr. Xiucong Sun	School of Astronautics, Beihang University	China
11		Attainable Landing Area Computation of Lunar Landers with Pseudo-Spectral and Polynomial based Guidance Methods	15	confirmed	Mr. Mohammad Alsharif	University of Bremen	Germany
12		Ionospheric path delay model for real time CDGPS-based baseline estimation for LEO satellites	15	withdrawn	Ms. Flavia Causa	University of Naples "Federico II"	Italy