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    Title

    Virtual Presentations - IAF ASTRODYNAMICS SYMPOSIUM

    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.

    IPC members
    • Co-Chair: Prof. Anna Guerman, Centre for Mechanical and Aerospace Science and Technologies (C-MAST), Portugal;

    • Co-Chair: Prof. Daniel Scheeres, Colorado Center for Astrodynamics Research, University of Colorado, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Attitude Control and Determination Accuracy Study of Small Satellite with Limited Set of Sensors

    confirmed

    Dr. Danil Ivanov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    Analytical guidance scheme for optimizing the orbital elements of low-thrust trajectories.

    Mr. Zhaowei Wang

    Tsinghua University, Beijing

    China

    capability analysis for manipulator-actuated integrated translational and rotational control strategy of spacecraft

    confirmed

    Dr. Feng Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    Chandrayaan-2: Orbit Maneuver Operations

    confirmed

    Mr. KOTA MALLESH BABU

    ISTRAC/ISRO

    India

    Development of an Unscented Kalman Filter for the validation of the European Space Agency candidate mission Asteroid Impact Mission’s optical navigation strategy up to Hardware In the Loop

    confirmed

    Mr. Aurelio Kaluthantrige

    International Space University

    France

    Differential-algebra Accelerated Poincaré Map of CR3BP and Its Application in Searching for Halo Orbits

    confirmed

    Ms. Xue Bai

    Beihang University

    China

    Fault detection and isolation method of redundant inertial measurement unit for slowly-varying fault based on neural network

    withdrawn

    Dr. Tong ZHANG

    Northwestern Polytechnical University

    China

    FULL - BODY RELATIVE SPACECRAFT MOTION. A MINIMAL PARAMETERIZATION USING CAYLEY-LIKE TRANSFORM

    confirmed

    Prof. Daniel Condurache

    Technical University of Iasi

    Romania

    Geosynchronous Longitude Measurements for Satellite Maneuver Detection

    confirmed

    Mr. Thomas Roberts

    Massachusetts Institute of Technology (MIT)

    United States

    Hardware-in-the-loop Testing of Nonlinear Control for Nanosatellite Formation Flying

    withdrawn

    Mr. Mohd Bilal

    University of Würzburg

    Germany

    Initial Orbit Improvement and Best Observation Time Window Determination Based-on Angles-Only Measurements

    Dr. Weihua Ma

    National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University

    China

    J2-perturbed low-energy orbits around Enceladus

    confirmed

    Dr. Francisco Salazar

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    Moon nanosatellite constellation connected by tethers

    withdrawn

    Mr. Guilherme Parreira Moia

    UNESP - São Paulo Sate University

    Brazil

    Motion and Parameter Estimation for tumbling non-cooperative targets using multiple satellite formation

    withdrawn

    Mr. Di Zhao

    Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics

    China

    Orbital stability analysis around the primary of a binary asteroid system

    confirmed

    Mr. Tao Fu

    Beihang University

    China

    regularized analytical orbit theory with solar radiation pressure

    confirmed

    Dr. Harishkumar Sellamuthu

    AgniKul Cosmos

    India

    Solar-Sail-Based Cislunar Navigation Constellation: Bounded Trajectories by Hamiltonian Structure-Preserving Control

    confirmed

    Ms. Xiaoyu Zuo

    Beihang University

    China