session IP

Title: Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM
type: interactive
Description: This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Astrodynamics addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.
Date: 2018-10-04
Time: 13:15
Room: IP Hall

IPC members

Co-Chair: Dr. Alfred Ng, Canadian Space Agency, Canada;
Co-Chair: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Wave-based motion control of flexible space systems	10	confirmed	Prof.Dr. William O'Connor	University College Dublin (UCD)	Ireland
Multispectral Image Processing for Navigation Using Low Performance Computing	10	confirmed	Mr. Duarte Rondao	Cranfield University	United Kingdom
Design of on-board fuel-oxidizer mass estimation algorithm for TeamIndus Lunar landing mission	10	withdrawn	Ms. Deepana Gandhi	Team Indus, Axiom Research Labs Pvt. Ltd.	India
Vision based state estimation using a graph-SLAM approach for proximity operations near an asteroid	10	confirmed	Mr. Arunkumar Rathinam	University of New South Wales	Australia
Fault tolerant attitude control for spacecraft with Lorenz and Magnetic Torques	10	withdrawn	Mr. Fuzhen Zhang	School of Astronautics, Beihang University, Beijing 100191, PR China	China
Invariant structures related to long term confinement of captured asteroids in the Earth-Moon system	10	withdrawn	Dr. Priscilla Sousa Silva	São Paulo State University - Universidade Estadual Paulista (UNESP)	Brazil
Evaluation of a camera-based pose and shape reconstruction technique for an unknown tumbling target	10	confirmed	Mr. Renato Volpe	Sapienza University of Rome	Italy
highly accurate guidance algorism for landing on a planet with gravity	10	confirmed	Mr. Toyonori Kobayakawa	Mitsubishi Heavy Industries, Ltd.	Japan
The Aldrin Cycler Improved by the Lorentz Force	10	confirmed	Mrs. Florence Duveiller	Georgia Institute of Technology, Atlanta	United States
GRACE accelerometer calibration by high precision non-gravitational force modelling and its validation	10	confirmed	Mr. Florian Wöske	Center of Applied Space Technology and Microgravity	Germany
Orbit Determination of CE-4’s Relay Satellite in Earth-Moon L2 Libration Point Orbit	10	withdrawn	Mr. jianfeng duan	Tsinghua University, Beijing	China
Control of 6DOF Spacecraft Hovering about Asteroids without Velocity Measurements	10	confirmed	Prof. Haichao Gui	Beihang University	China
Relative State Measurement of A Non-Cooperative Spacecraft for Final Approaching Stage of On-Orbit Servicing Using Contour Features	10	confirmed	Dr. Yunhua Wu	Nanjing University of Aeronautics and Astronautics	China
Chaotic motions of tethered tug-debris system with fuel residuals	10	confirmed	Prof. Vladimir S. Aslanov	Samara National Research University (Samara University)	Russian Federation
autonomous guidance using nonlinear model predictive control for rendezvous and docking with non-cooperative targets	10	confirmed	Mr. RaviKumar L	ISRO Satellite Centre (ISAC)	India
Distributed Coordination Control for Multiple Spacecraft with Coupled Attitude and Orbit Dynamics under the Directed Graph	10	confirmed	Prof. Ma Weihua	National Key Laboratory of Aerospace Flight Dynamic, Northwestern Polytechnical University	China
dual quaternion based relative navigation for spacecraft proximity operation	10	confirmed	Ms. Yunju Na	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
Inverse-dynamics Particle Swarm Optimization for Real Time Optimal Control: Challenges and Opportunities	10	confirmed	Dr. Dario Spiller	Sapienza University of Rome	Italy
Space-oriented navigation solutions with integrated sensor-suite: the I3DS H2020 project	10	confirmed	Dr. Antonio Fulvio Scannapieco	Cranfield University	United Kingdom
Investigation into the Controllability of Underactuated Magnetically Stabilized Spacecraft	10	confirmed	Mr. Mike Alger	Ryerson University	Canada
End-of-life disposal design for spacecraft at Libration Points Orbits and an interpretation of their probability of Earth return	10	confirmed	Ms. Greta De Marco	Politecnico di Milano	Italy
HIGHER-ORDER CAYLEY TRANSFORM FOR RELATIVE POSE PARAMETERIZATION OF SPACECRAFT	10	confirmed	Prof. Daniel Condurache	Technical University of Iasi	Romania
Novel orbit improvement method through pseudo relative motion analysis	10	confirmed	Dr. Mingtao Li	1: National Space Science Center, Chinese Academy of Sciences; 2:University of Chinese Academy of Sciences	China
sentinel-3 tandem: from concept to implementation	10	confirmed	Mr. Berthyl Duesmann	ESA - European Space Agency	The Netherlands
The Borea project: a quadrotor UAV cradle-to-grave design for space GNC prototyping and testing	10	confirmed	Mr. Luigi Colangelo	Politecnico di Torino	Italy
Parameter Determination of Dynamical Systems Using Chaotic Orbits	10	withdrawn	Mr. Jorge Nicolás-Alvarez	Universitat Politecnica de Catalunya (UPC)	Spain
Orbital and Formation Optimization for Space Gravitational Waves Observatory Mission	10	confirmed	Dr. Mingtao Li	1: National Space Science Center, Chinese Academy of Sciences; 2:University of Chinese Academy of Sciences	China
Next steps for the CryoSat-2 mission: Improving sea-ice estimates in joint operations with the ICESat-2 spacecraft.	10	confirmed	Mr. Javier Sanchez	ESA - European Space Agency	Germany
Missions for Asteroid Insertion into Earth-Mars Cycler	10	confirmed	Dr. Francesco Simeoni		Italy
Mission Design and Analysis for Mars and Phobos Missions via Lunar and Mars-Phobos Distant Retrograde Orbits	10	confirmed	Mr. Davide Conte	Pennsylvania State University	United States
Fuel-optimal trajectories near Lagrange points	10	confirmed	Mr. Florent Bréhard	LAAS-CNRS	France
Advanced In-Flight Results from the GPS Receiver on SmallGEO	10	confirmed	Mr. Nils Neumann	OHB System AG-Bremen	Germany
advanced approach based on convex programming for mars powered descent guidance	10	confirmed	Mr. Kazuya Echigo	Department of Engineering, The University of Tokyo	Japan
Extended reactionless workspace of a space manipulator through reaction wheels	10	confirmed	Mr. Alessandro Tringali	Space Mechatronic Systems Technology Laboratory, University of Strathclyde	United Kingdom
The mission's design of a solar sail spacecraft to the nearest circumsolar space, based on a locally-optimal control laws	10	confirmed	Prof. Olga Starinova	Samara National Research University (Samara University)	Russian Federation
How to Send a Signal to Fixed Ground Antennas from a Non-Geostationary Satellite	10	confirmed	Mr. Dominik Quantius	Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)	Germany
Proba-3 Mission: In orbit demonstration of a high performance relative position and attitude control	10	confirmed	Mr. Daniel Serrano	SENER Ingenieria y Sistemas, S.A.	Spain
Coordinated Capture of a Passive Space Object Using Augmented State Estimation and Neural Networks	10	confirmed	Mrs. Emily Gleeson	Ryerson University	Canada

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