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  • session IP

    Title

    Interactive Presentations

    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

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Performance analysis of Fast Unscented Kalman Filters for Attitude Determination in UNSW-EC0 CubeSat Engineering Model

    withdrawn

    Mr. Sanat Biswas

    UNSW Australia

    Australia

    2

    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

    3

    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

    4

    Orbital transfers around a double asteroid system

    confirmed

    Mr. Geraldo Oliveira

    Federal Center for Technological Education of Minas Gerais

    Brazil

    5

    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

    6

    Safety Trajectory Optimization in Ultra-close Proximity to Large Debris

    confirmed

    Ms. Xiaoyu Chu

    Beijing Institute of Technology

    China

    7

    Quaternion based Attitude Stabilization in the Circular Restricted Three-Body Problem

    confirmed

    Mr. Yuki Akiyama

    Kyushu University

    Japan

    8

    High Accuracy and High Stability Pointing of Space Telescope Based on Ultra-Quiet Platform

    confirmed

    Dr. Guangde Xu

    CAST

    China

    9

    Late-Life Reconfiguration Maneuvers of the RapidEye Constellation for the Reversal of LTAN Drift

    confirmed

    Dr. Jesse Eyer

    Planet Labs Inc.

    Germany

    10

    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

    11

    The combined Lambert-Tisserand resolution applied to the single flyby problem

    confirmed

    Mr. Davide Menzio

    Politecnico di Milano

    Italy

    12

    Goal-oriented planning and path parameterization for time-optimal spacecraft reorientation

    confirmed

    Mr. Hui Wang

    Beijing Institute of Technology

    China

    13

    three-channel filter theory for fault detection and isolation of redundant inertial measurement unit

    confirmed

    Dr. Tong ZHANG

    Northwestern Polytechnical University

    China

    14

    relative navigation filter algorithm for elliptical orbits based on onboard relative measurements

    confirmed

    Mr. Fan Wu

    Harbin Institute of Technology

    China

    15

    A Novel Velocity Observer for 6DOF Spacecraft Formation Flying

    withdrawn

    Dr. Haichao Gui

    Ryerson University

    Canada

    16

    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

    17

    Periodic orbits in the Restricted Three-Body Problem with non-spherical mass distribution of primaries

    withdrawn

    Dr. Fabio Ferrari

    Politecnico di Milano

    Italy

    18

    Delta-V Assisted Homoclinic and Heteroclinic Connections of Periodic Orbits around Natural Equilibrium Points of Irregular Asteroids

    withdrawn

    Mr. Hongwei YANG

    Tsinghua University

    China

    19

    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

    20

    safety analysis for near rectilinear orbit close approach rendezvous in the circular restricted three-body problem

    confirmed

    Mr. Antonino Campolo

    Politecnico di Milano

    Italy

    21

    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

    22

    Software Architecture for Deep-Space Navigation Filter Development

    confirmed

    Mr. Andrew Harris

    Colorado Center for Astrodynamics Research, University of Colorado

    United States

    23

    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

    24

    Low-Orbit Spacecraft Service Planning

    confirmed

    Prof. Yury Razoumny

    Peoples's Friendship University of Russia (RUDN)

    Russian Federation

    25

    AOCS Design and On-orbit Performance of ARASE/ERG Satellite

    confirmed

    Dr. Toshio Kamiya

    NEC Corporation Space Systems Div.

    Japan

    26

    Preliminary Study on Vertical Descent Guidance for Precise Lunar Landing

    confirmed

    Mr. Takahiro Ito

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    27

    A Fiber Optic Gyro-Based Attitude Control System for Autonomous Target Tracking

    withdrawn

    Mr. Elias Solorzano

    Space Flight Laboratory, University of Toronto

    Canada

    28

    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

    29

    Model and trajectory optimization for an ideal laser-enhanced solar sail

    confirmed

    Prof. Bernd Dachwald

    FH Aachen University of Applied Sciences

    Germany

    30

    optimization of flyby schemes in the framework of adr mission in leo

    confirmed

    Mr. Dmitriy Grishko

    Bauman Moscow State Technical University

    Russian Federation

    31

    Comparative Assessment of Different Constellation Geometries for Space-based Applications

    confirmed

    Ms. Simeng Huang

    Politecnico di Milano

    Italy

    32

    Matching of Patched–Integrated Trajectories for Cis-Lunar Transfers

    confirmed

    Mr. Yat Hei Ng

    The Hong Kong University of Science and Technology

    Hong Kong

    33

    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

    34

    Characterisation of the geopotential deficiencies in SGP4 propagation for drag-less low-earth orbiting test cases

    withdrawn

    Mr. Richard Samuel

    Australia

    35

    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

    36

    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