IAF Digital Library

8

session 8

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: 2019-10-25
Time: 09:45
Room: 150A

IPC members

Co-Chair: Prof. Yong Chun Xie, Beijing Institute of Control Engineering, China Academy of Space Technology (CAST), China;
Co-Chair: Dr. Anton de Ruiter, Ryerson University, Canada;
Rapporteur: Mr. Miguel Bello Mora, Deimos Space S.L., Spain;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	09:45	GNC Architecture for an Optimal Rendezvous to an Uncooperative Tumbling Target Using Passive Monocular Camera	15	confirmed	Mr. Renato Volpe	Sapienza University of Rome	Italy
2	10:00	Linear Covariance Analysis for the Final Rendezvous Phase of the Mars Sample Return – Earth Return Orbiter Mission	15	withdrawn	Mr. Francesco Capolupo	Airbus Defence and Space	France
3	10:15	Autonomous Orbit Control with on-board collision risk management for Low-Earth Orbit Satellites	15	confirmed	Mr. Jerome Thomassin	Centre National d'Etudes Spatiales (CNES)	France
4	10:30	Dual Quaternion Based Autonomous Rendezvous and Docking Via Model Predictive Control	15	confirmed	Mr. Burak Omer Iskender	Nanyang Technological University	Singapore, Republic of
5	10:45	Nonlinear control with J2 and drag perturbations for nanosatellite formation flight	15	confirmed	Mr. Roland Haber	Zentrum für Telematik	Germany
6	11:00	Assessment and implementation of viable navigation filter options for close-proximity satellite operation using visual navigation	15	confirmed	Mr. Noel Weber	Deutsches Zentrum fuer Luft- und Raumfahrt (DLR)	Germany
7	11:15	ASTROBATIC: a hopping-maneuver experiment for a spacecraft-manipulator system on board the International Space Station	15	confirmed	Prof. Marcello Romano	Naval Postgraduate School	United States
8	11:30	Variable-Time-Domain Neighboring Optimal Guidance and Attitude Control of Low-Thrust Lunar Orbit Transfers	15	confirmed	Dr. Mauro Pontani	Sapienza University of Rome	Italy
9	11:45	Distributed robust consensus-based control with collision avoidance for satellite formation flying	15	confirmed	Mr. Roland Haber	Zentrum für Telematik	Germany
10	12:00	Energy-Optimal Rendezvous Spacecraft Guidance via Theory of Connections	15	confirmed	Prof. Roberto Furfaro	University of Arizona	United States
11	12:15	Robust formation control in Low-Earth-Orbit using sector bounds for J2 and drag disturbances	15	withdrawn	Mr. Florian Kempf	University of Würzburg	Germany
12	12:30	Fuel-Efficient Formation Flying of an Observatory and External Occulter in the Circular Restricted Three-Body Problem	15	confirmed	Mr. William Sanchez	Massachusetts Institute of Technology (MIT)	United States