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  • session 5

    Title

    Guidance, Navigation & Control (3)

    Description

    The emphasis of this theme is on the studies and application related to the guidance, navigation and control of Earth-orbiting and interplanetary spacecraft, including formation flying, rendezvous and docking.

    Date

    2023-10-05

    Time

    15:00

    Room

    BCC B4

    IPC members
    • Co-Chair: Prof.Dr. Jean de Lafontaine, NGC Aerospace Ltd., Canada;

    • Co-Chair: Dr. Yung Fu Tsai, National Cheng Kung University, Taiwan, China;

    • Rapporteur: Dr. Miguel Bello Mora, Deimos Space SLU, Spain;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:00

    Design and verification of a robust drag-free attitude control system for the LISA mission

    15

    withdrawn

    Dr. Joost Veenman

    SENER Aeroespacial

    Spain

    2

    15:15

    Trajectory Optimization, Guidance and Control of Low-Thrust Orbit Transfers from the Lunar Gateway to Low Lunar Orbits

    15

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    3

    15:30

    The EXTREMA Autonomous Guidance Algorithm for Low-Thrust Interplanetary Spacecraft

    15

    confirmed

    Mr. Andrea Carlo Morelli

    Politecnico di Milano

    Italy

    4

    15:45

    On the dynamics and control of a spacecraft observing exoplanets via the Solar Gravitational Lens

    15

    confirmed

    Mr. Denis Perepukhov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    5

    16:00

    KAMnet – Applying Machine Learning Techniques for Optical Navigation in Earth Observation Missions

    15

    confirmed

    Dr. Manuel Sanjurjo-Rivo

    Universidad Carlos III de Madrid

    Spain

    6

    16:15

    Robustness to Noise Analysis of Solar Sailing Adaptive Control with Solar Flux Estimation Using Finite Excitation

    15

    withdrawn

    Dr. Riccardo Bevilacqua

    Embry-Riddle Aeronautical University

    United States

    7

    16:30

    Universal Function and Primer Vector Theory for Fuel-optimal Lambert Problem

    15

    confirmed

    Dr. Feng Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    8

    16:45

    A new form of osculating Keplerian approximation of N-Body non-Keplerian motion for the design of GNC algorithms

    15

    confirmed

    Mr. Catello Leonardo Matonti

    Politecnico di Torino

    Italy

    9

    17:00

    OpNav-Only Station Keeping on NRHO using Stochastic Predictive Control

    15

    confirmed

    Mr. Yuri Shimane

    Georgia Institute of Technology

    United States

    10

    17:15

    Particle Swarm Optimization based Tracking Window Planning for Cislunar Orbiters Performing Autonomous Radiometric Navigation

    15

    confirmed

    Mr. Erdem Turan

    Delft University of Technology (TU Delft), The Netherlands

    The Netherlands