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  • session 4

    Title

    Guidance, Navigation and Control (2)

    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

    2024-10-18

    Time

    10:15

    Room

    Blue Hall 2

    IPC members
    • Co-Chair: Dr. Mai Bando, Kyushu University, Japan;

    • Co-Chair: Prof. Eberhard Gill, Delft University of Technology, The Netherlands;

    • Rapporteur: Prof. Hanspeter Schaub, Colorado Center for Astrodynamics Research, University of Colorado, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Optimal Guidance Control Considering Multiple Constraints for Asteroid Sample Return

    15

    confirmed

    Prof. Toshio Kamiya

    Meisei University

    Japan

    2

    10:30

    study on onboard explicit celestial descent guidance using receding horizon control adaptable in microgravity environments

    15

    confirmed

    Mr. Kent Yoshikawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    10:45

    On-orbit operation results of the powered descent guidance algorithm for pinpoint lunar landing

    15

    confirmed

    Mr. Satoshi Ueda

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    11:00

    The Development and Verification Method of SLIM Lunar Landing Navigation Algorithms

    15

    confirmed

    Mr. Kentaro Watanabe

    Mitsubishi Electric Corporation

    Japan

    5

    11:15

    Integrated Optical Terrain Relative Navigation for Autonomous Lunar Landing

    15

    confirmed

    Mr. Giovanni Pio Parracino

    Politecnico di Milano

    Italy

    6

    11:30

    High-fidelity Optimal Control Laws to Characterize the Maneuvering Capabilities of Earth-bound Solar Sails

    15

    confirmed

    Mr. Livio Carzana

    Delft University of Technology (TU Delft)

    The Netherlands

    7

    11:45

    Fuel-Optimal Trajectories of the Perturbed Circular Restricted Three-Body Problem for Lunar Occultation Applications

    15

    confirmed

    Mr. Luis Mendoza Zambrano

    Embry-Riddle Aeronautical University

    United States

    8

    12:00

    Design of Minimum-Time Low-Thrust Transfer between Quasi-Periodic Orbits

    15

    confirmed

    Mr. Naoki Hiraiwa

    Kyushu University

    Japan

    9

    12:15

    analysis of periodic and quasi-periodic orbits with optimal feedback control

    15

    confirmed

    Ms. Ayano Tsuruta

    Kyushu University

    Japan

    10

    12:30

    Spacecraft trajectory optimisation using Differential Dynamic Programming

    15

    confirmed

    Mr. Pietro Mondino

    ISAE - Institut Supérieur de l'Aéronautique et de l'Espace

    France

    1*

    10:15

    Observability-based orbiter aided cooperative navigation for asteroid landing

    15

    confirmed

    Dr. Wenbo Xiu

    Beijing Institude of technology

    China

    2*

    10:30

    Model Predictive Control Strategy with a Decreasing Horizon Interval for a Reusable Launcher in a Landing Scenario

    15

    confirmed

    Mr. Guillermo Zaragoza Prous

    Cranfield University

    United Kingdom

    3*

    10:45

    RCDs-based feedback control of a solar sail spacecraft at the Earth-Sun L1 point with dual pointing requirements

    15

    confirmed

    Mr. Hongyi Xie

    Politecnico di Milano

    Italy

    4*

    11:00

    Robust Powered Descent Guidance Using Successive Convexification and Tube Model Predictive Control

    15

    confirmed

    Mr. Duozhi Gao

    Harbin Institute of Technology

    China

    5*

    11:15

    Long-Term Station Keeping around Earth-Moon Synodic Resonant Halo Orbits Using Solar Sails in High-Fidelity Dynamics Model

    15

    confirmed

    Dr. Toshihiro Chujo

    Tokyo Institute of Technology

    Japan