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  • session 1

    Title

    Orbital Dynamics (1)

    Description

    This theme discusses advances in the knowledge of natural motions of objects in orbit around the Earth, planets, minor bodies, Lagrangian points and more generally natural orbital dynamics of spacecraft in the Solar System. It also covers advances in orbit determination.

    Date

    2018-10-01

    Time

    15:00

    Room

    CCB Borgward

    IPC members
    • Co-Chair: Prof. Gerard Gomez, University of Barcelona, Spain;

    • Co-Chair: Dr. Antonio Prado, National Institute for Space Research - INPE , Brazil;

    • Rapporteur: Mr. Al Cangahuala, National Aeronautics and Space Administration (NASA), Jet Propulsion Laboratory, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Higher order analytical solution to the Distant Retrograde orbits problem

    15

    confirmed

    Dr. Martin Lara

    Universidad de La Rioja

    Spain

    2

    15:15

    Hybrid SGP4 propagator based on machine-learning techniques applied to GALILEO-type orbits

    15

    confirmed

    Dr. Juan Félix San-Juan

    Universidad de La Rioja

    Spain

    3

    15:30

    high accuracy orbit determination of geo-stationary satellites using differential algebra and high-order extended kalman filter

    15

    confirmed

    Mr. Jianlin Chen

    National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University

    China

    4

    15:45

    Analytical and semi-analytical approaches to the third-body perturbation in nearly co-orbital regimes

    15

    confirmed

    Ms. Rita Neves

    Cranfield University

    United Kingdom

    5

    16:00

    Accurate tour trajectory design for the Jovian system using Pseudo-state theory

    15

    withdrawn

    Dr. Yang Bin

    Nanjing University of Aeronautics and Astronautics,

    China

    6

    16:15

    Trajectory design connecting invariant manifolds of periodic orbits with continuous low-thrust

    15

    withdrawn

    Mr. YUKI OSHIMA

    Kyushu University

    Japan

    7

    16:30

    Efficient two-body approximations of impulsive transfers between Halo orbits

    15

    confirmed

    Dr. Elena Fantino

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    8

    16:45

    identifying heteroclinic transfers using artificial neural networks

    15

    confirmed

    Mr. Stijn De Smet

    University of Colorado Boulder

    United States

    9

    17:00

    Extended State Space Approach for Trajectory Design in Elliptic Restricted Three-Body Problem

    15

    confirmed

    Dr. Yuki Akiyama

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    10

    17:15

    Dynamics of capture orbits from libration region analysis

    15

    confirmed

    Mr. Stefano Carletta

    Sapienza University of Rome

    Italy

    11

    17:30

    Phasing and rendezvous operations on non-Keplerian orbits in the Earth-Moon system

    15

    confirmed

    Mr. Lorenzo Bucci

    Politecnico di Milano

    Italy

    12

    17:45

    Neutral atmosphere drag at the altitude of LARES and Ajisai

    15

    confirmed

    Dr. Luciano Anselmo

    ISTI-CNR

    Italy

    13

    18:00

    Analytical solution of low-thrust minimum energy coplanar orbit transfer by using time-averaged canonical equations

    15

    confirmed

    Mr. Kenji Kitamura

    Mitsubishi Electric Corporation

    Japan

    14

    18:15

    Osculating to mean element transformation for accurate re-entry prediction with semi-analytical methods

    15

    withdrawn

    Dr. Martin Lara

    Universidad de La Rioja

    Spain