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  • session 3

    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.

    IPC members
    • Co-Chair: Dr. Miguel Bello Mora, Deimos Space SLU, Spain;

    • Co-Chair: Prof. Igor V. Belokonov, Samara National Research University (Samara University), Russian Federation;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Mars Sample Return: ERO Navigation and guidance during the inbound leg

    10

    confirmed

    Mr. Pablo Hermosin

    Deimos Space SLU

    Spain

    3

    A sparse nonlinear model predictive control for autonomous space missions

    10

    confirmed

    Mr. Michele Pagone

    Politecnico di Torino

    Italy

    4

    Generation and Stability Analysis of Bounded Relative Orbits Using Lagrangian Coherent Structures

    10

    confirmed

    Dr. Yanchao He

    DFH Satellite Co., Ltd.

    China

    5

    improving satellite on-board orbit estimation with artificial neural networks

    10

    confirmed

    Mr. Sergiu-Ştefan Mihai

    Romanian InSpace Engineering SRL

    Romania

    6

    Nonlinear Modelling and drag-free controller design for space-based gravitational wave detector

    10

    confirmed

    Mr. Haojun Ma

    University of Chinese Academy of Sciences

    China

    9

    Finite-time reachability of thrust-less rendezvous mission under input constraints

    10

    confirmed

    Mr. Mohamed Shouman

    Kyushu University

    Japan

    10

    Integrated Strategy of Stationkeeping, Autonomous Navigation and Real-time Geodetical Recovery of Gravity Fields: Application into Interplanetary Trajectory Correction Maneuver of Cassini Mission

    10

    confirmed

    Ms. Yaru Zheng

    Beihang University

    China

    12

    Low-thrust nonlinear orbit control using nonsingular equinoctial elements

    10

    confirmed

    Mr. Marco Pustorino

    Sapienza University of Rome

    Italy

    13

    System requirements analysis for JAXA's contribution to Comet Interceptor Mission: Autonomous Navigation, Guidance and Attitude Control for a Hyperbolic Comet Fly-by

    10

    confirmed

    Mr. Pablo Machuca

    Cranfield University

    United Kingdom

    14

    Formation Flying L-band Aperture Synthesis: design challenges and innovative formation architecture concept

    10

    confirmed

    Ms. Francesca Scala

    Politecnico di Milano

    Italy

    15

    3U Cubesat aerodynamic design aimed to increase attitude stability and orbital lifetime

    10

    confirmed

    Prof. Vladimir S. Aslanov

    Samara National Research University (Samara University)

    Russian Federation

    16

    Methodology of in-flight parameter identification for the nanosatellite angular motion mathematical model under a priori uncertainty

    10

    confirmed

    Prof. Igor V. Belokonov

    Samara National Research University (Samara University)

    Russian Federation