session IP

Title: Interactive Presentations
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 eight 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: 2017-09-28
Time: 12:45
Room: Hall J&K2

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	Presentation status	Speaker	Affiliation	Country
Performance analysis of Fast Unscented Kalman Filters for Attitude Determination in UNSW-EC0 CubeSat Engineering Model	withdrawn	Mr. Sanat Biswas	UNSW Australia	Australia
Analysis of orbits near a binary asteroid system modeled as rotating mass dipoles	confirmed	Dr. Antonio Fernando Bertachini Almeida Prado	Instituto Nacional de Pesquisas Espaciais (INPE)	Brazil
A New Type of Sun Sensor for Micro-Satellite Based on Bionic Compound Eye	confirmed	Dr. Yunhua Wu	Nanjing University of Aeronautics and Astronautics	China
Orbital transfers around a double asteroid system	confirmed	Mr. Geraldo Oliveira	Federal Center for Technological Education of Minas Gerais	Brazil
Study on the Stability of Nonlinear Time-varying Spacecraft Control System	confirmed	Prof. Yong Chun Xie	Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)	China
Safety Trajectory Optimization in Ultra-close Proximity to Large Debris	confirmed	Ms. Xiaoyu Chu	Beijing Institute of Technology	China
Quaternion based Attitude Stabilization in the Circular Restricted Three-Body Problem	confirmed	Mr. Yuki Akiyama	Kyushu University	Japan
High Accuracy and High Stability Pointing of Space Telescope Based on Ultra-Quiet Platform	confirmed	Dr. Guangde Xu	CAST	China
Late-Life Reconfiguration Maneuvers of the RapidEye Constellation for the Reversal of LTAN Drift	confirmed	Dr. Jesse Eyer	Planet Labs Inc.	Germany
Planetary UAV exploration simulated in a flying arena with the use of novel dual quaternions attitude dynamics algorithms	withdrawn	Mr. Andrea Antonello	CISAS – “G. Colombo” Center of Studies and Activities for Space, University of Padova	Italy
The combined Lambert-Tisserand resolution applied to the single flyby problem	confirmed	Mr. Davide Menzio	Politecnico di Milano	Italy
Goal-oriented planning and path parameterization for time-optimal spacecraft reorientation	confirmed	Mr. Hui Wang	Beijing Institute of Technology	China
three-channel filter theory for fault detection and isolation of redundant inertial measurement unit	confirmed	Dr. Tong ZHANG	Northwestern Polytechnical University	China
relative navigation filter algorithm for elliptical orbits based on onboard relative measurements	confirmed	Mr. Fan Wu	Harbin Institute of Technology	China
A Novel Velocity Observer for 6DOF Spacecraft Formation Flying	withdrawn	Dr. Haichao Gui	Ryerson University	Canada
Coordinated Path Planning Strategy for Dual-Arm Space Robot Using B Spline	confirmed	Dr. Mingming Wang	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University	China
Periodic orbits in the Restricted Three-Body Problem with non-spherical mass distribution of primaries	withdrawn	Dr. Fabio Ferrari	Politecnico di Milano	Italy
Delta-V Assisted Homoclinic and Heteroclinic Connections of Periodic Orbits around Natural Equilibrium Points of Irregular Asteroids	withdrawn	Mr. Hongwei YANG	Tsinghua University	China
Large-Scale Spacecraft Swarm Decentralized Formation Flying Control Based on Sliding Mode Control and Tracking Differentiator	confirmed	Mr. Jinfeng Sun	School of Transportation Science and Engineering, Beihang University, Beijing, 100191, PR China	China
safety analysis for near rectilinear orbit close approach rendezvous in the circular restricted three-body problem	confirmed	Mr. Antonino Campolo	Politecnico di Milano	Italy
Novel Direct Method for Continuous Thrust Trajectory Optimization	confirmed	Dr. Mingtao Li	1: National Space Science Center, Chinese Academy of Sciences; 2:University of Chinese Academy of Sciences	China
Software Architecture for Deep-Space Navigation Filter Development	confirmed	Mr. Andrew Harris	Colorado Center for Astrodynamics Research, University of Colorado	United States
The Homoclinic and Heteroclinic Connections of Planar Symmetric Resonant Orbits in the Restricted Three-Body Earth-Moon System	confirmed	Mr. Chao Peng	Chinese Academy of Sciences	China
Low-Orbit Spacecraft Service Planning	confirmed	Prof. Yury Razoumny	RUDN University	Russian Federation
AOCS Design and On-orbit Performance of ARASE/ERG Satellite	confirmed	Dr. Toshio Kamiya	NEC Corporation Space Systems Div.	Japan
Preliminary Study on Vertical Descent Guidance for Precise Lunar Landing	confirmed	Mr. Takahiro Ito	Japan Aerospace Exploration Agency (JAXA)	Japan
A Fiber Optic Gyro-Based Attitude Control System for Autonomous Target Tracking	withdrawn	Mr. Elias Solorzano	Space Flight Laboratory, University of Toronto	Canada
Using the spacecraft with a solar sail to monitor a specific area of Mars	confirmed	Prof. Olga Starinova	Samara National Research University (Samara University)	Russian Federation
Model and trajectory optimization for an ideal laser-enhanced solar sail	confirmed	Prof. Bernd Dachwald	FH Aachen University of Applied Sciences	Germany
optimization of flyby schemes in the framework of adr mission in leo	confirmed	Mr. Dmitriy Grishko	Bauman Moscow State Technical University	Russian Federation
Comparative Assessment of Different Constellation Geometries for Space-based Applications	confirmed	Ms. Simeng Huang	Politecnico di Milano	Italy
Matching of Patched–Integrated Trajectories for Cis-Lunar Transfers	confirmed	Mr. Yat Hei Ng	The Hong Kong University of Science and Technology	Hong Kong SAR, China
Searching Reachable Region of Low-Thrust Trajectories by Superposition and Greedy Optimization	confirmed	Mr. Albert Wai Kit Lau	The Hong Kong University of Science and Technology	Hong Kong SAR, China
Characterisation of the geopotential deficiencies in SGP4 propagation for drag-less low-earth orbiting test cases	withdrawn	Mr. Richard Samuel		Australia
RELATIVE REACHABLE DOMAIN COMPUTING OF SPACECRAFT WITH SINGLE IMPULSE IN MISSING PERIOD	withdrawn	Mr. Junhua Zhang	National Key Laboratory of Aerospace Flight Dynamic, Northwestern Polytechnical University	China
The integrated dynamics modeling and coupling analysis for orbit and attitude of spacecrafts	confirmed	Prof. Weihua Ma	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi’an	China

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