session IP

Title: Interactive Presentations
type: interactive
Description: Authors with an abstract accepted for an interactive presentation will be asked to prepare slides and display them for the duration of the congress on plasma screens. Authors will be assigned to interactive sessions in which they must be near the plasma screens to engage in interactive discussions with other congress attendees.
Date: 2016-09-28
Time: 13:15
Room: Jalisco Hall C - Exhibition Hall

IPC members

Coordinator: Mr. Christophe Bonnal, European Conference for Aero-Space Sciences (EUCASS), France;
Coordinator: Dr. Darren McKnight, LeoLabs, United States;
Coordinator: Prof. Tetsuo Yasaka, Institute for Q-shu Pioneer of Space, Inc. (iQPS), Japan;

papers
Paper title	Presentation status	Speaker	Affiliation	Country
Steady State Heat Transfer Experiments in the Slip Regime Using the Oxford Low Density Wind Tunnel	withdrawn	Mr. Nathan Donaldson	University of Oxford	United Kingdom
Tethered Systems for Space Debris Removal: the TedDy project	withdrawn	Ms. Laura Costanza	Aviospace S.R.L	Italy
Adaptive remediation of the space debris environment using feedback control	confirmed	Mr. Gian Luigi Somma	University of Southampton	United Kingdom
Quick Methods of Planning of Observation Sessions of Orbital Objects Implemented by Space Vehicles		Ms. Tatyana V. Labutkina	Dnepropetrovsk National University named after Oles' Gonchar	Ukraine
Expansion of the Notion of a Mechanical Conflict of Orbital Objects: a Serial Conflict and a Polyconflict, Fast Methods of Forecasting Them		Ms. Tatyana V. Labutkina	Dnepropetrovsk National University named after Oles' Gonchar	Ukraine
COLLISION-FREE PATH PLANNING OF SPACE ROBOT FOR MULTIPLE TASKS	confirmed	Ms. Suping Zhao	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an	China
Evaluation of drag augmentation system design requirements for a wide range of small LEO satellite platforms	withdrawn	Ms. Chiara Palla	Cranfield University	United Kingdom
FORTE: ISON Robotic Telescope Control Software	withdrawn	Dr. Vladimir Kouprianov	Central Astronomical Observatory of the Russian Academy of Sciences	Russian Federation
Use of an Optimisation Technique for the Correlation of Aerothermal Data on Geometric Primitives for Debris Demise Calculations	withdrawn	Mr. Nathan Donaldson	University of Oxford	United Kingdom
Space Debris Events Analysis Platform and Its Application	confirmed	Mr. You cheng Yu	National Astronomical Observatories, Chinese Academy of Sciences	China
Feasibility Study of Active Debris Removal using Hybrid Propulsion System	confirmed	Dr. Stefania Tonetti	Deimos Space SLU	Spain
Ballistic Limit Equations’ Predictive Indicators		Dr. Guanghui Jia	Beihang University	China
A light weight robot arm for capturing space debris	withdrawn	Dr. Shin-Ichiro Nishida	Tottori University	Japan
Damage of Quartz Glass under Hypervelocity Impact	withdrawn	Ms. Jie Huang	China Aerodynamics Research and Development Center (CARDC)	China
Applications of image deconvolution for optical space debris observation	confirmed	Mr. Rong-Yu Sun	Purple Mountain Observatory (PMO)	China
USE OF SPACE DEBRIS AS THE PROPULSIVE MASS FOR ROCKET ENGINES.	withdrawn	Mr. Oleg Aleksandrov	AVIASTAR Inc www.aviastar.us	United States
analysis of liris infrared imagery for active debris removal missions	withdrawn	Ms. Özgün YILMAZ	Cranfield University	United Kingdom
The automation of the EQUO On-Ground Observatory at Broglio Space Center for Space Surveillance	confirmed	Dr. Tommaso Cardona	University of Rome "La Sapienza"	Italy
Development of the Italian observatory network for Space Surveillance	confirmed	Dr. Gioacchino Scire	University of Rome "La Sapienza"	Italy
The ADAPS as a gradually developing ballistic data processing system	withdrawn	Mr. Viktor Voropaev	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
A Visual Perception and Intelligence Servo System Used for Spatial Debris Active Clearing Robots	confirmed	Dr. Shibo Gao	Beijing Aerospace Automatic Control Institute	China
Monitoring the Health of Geosynchronous Spacecraft Using Photometric Observations	confirmed	Mr. Toshiya Enomoto	Kyushu University	Japan
Environmental Impact of Space Debris Repositioning	confirmed	Dr. Claudio Bombardelli	Technical University of Madrid (UPM)	Spain
Vision based attitude determination using a Simultaneous Localization and Mapping algorithm during relative circumnavigation of non-cooperative objects	confirmed	Mr. Andrea Antonello	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
Using the Analytic Hierarchy Process in the assessment of the probability for an explosion to occur during the atmospheric re-entry	confirmed	Ms. Cristina De Persis	Trinity College	Ireland
The SOLEM Evolution Model and its uncertainty Analysis	withdrawn	Ms. xiaowei wang	National Astronomical Observatories, Chinese Academy of Sciences	China
e.deorbit – Elements of an ADR mission that require an in-orbit-demonstration and ways to achieve it	withdrawn	Mr. Marc Scheper	OHB System AG-Bremen	Germany
A Flexible and Adaptive Capture Device for Orbital Debris Removal Based on Octopus-Inspired Pneumatic Soft Robot	confirmed	Mr. Liangliang HAN	Institute of Aerospace System Engineering Shanghai, CASC	China
Computation and Dynamic Analysis of Deployment of Inflatable Membrane Structure for Debris Removal	confirmed	Mr. Benke Shi	Beihang University	China
evaluation of the impact resistance of glare under hypervelocity impact loading	withdrawn	Mr. Chunsen Shi	Delft University of Technology (TU Delft)	The Netherlands
Experiment and numerical simulation of hypervelocity impact on honeycomb by volcano rock simulacrum for micro-meteoroids	confirmed	Dr. Bin Jia	Harbin Institute of Technology	China
Stochastic Modeling of Hypervelocity Impacts including Momentum Enhancement in Attitude Propagation of Space Debris	confirmed	Prof. Inna Sharf	McGill University	Canada
dynamic programming and autonomous approach technology in on-orbit maintenance for micro satellite constellation	confirmed	Dr. Shan Lu	Shanghai Aerospace Control Technology Institute (SACTI), Shanghai Academy of Spaceflight Technology (SAST)	China
The research of tiny non-cooperative space target relative orbit determination with intermittent measurement information	withdrawn	Mr. Fei Han	Harbin Institute of Technology	China
International Space Situational Awareness System for Avoiding Orbital Collisions: Framework, Challenges and Recommendations	confirmed	Dr. Changfang Zhang	Center for National Security and Strategic Studies(CNSSS), National Unversity of Defense Technology (NUDT)	China
General framework for non-cooperative satellite's tumbling motion estimation using a single imaging sensor and an FPGA/DSP hardware platform	confirmed	Mr. Konrad Bojar	PIAP	Poland
The Nonlinearity Character of The Electrodynamic Tether	confirmed	Mr. Shohei Kudo	The University of Electro-Communications	Japan
The Process Analysis and Orbit Prediction of The Decaying Space Debris	withdrawn	Mr. Liu Yisi	Chinese Academy of Sciences	China

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