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  • session 1

    Title

    Guidance, Navigation and Control (1)

    type

    oral

    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

    2021-10-25

    Time

    15:15

    Room

    Sheikh Maktoum C

    IPC members
    • Co-Chair: Mr. Juan Carlos Bastante, OHB System AG-Bremen, Germany;

    • Co-Chair: Prof. Moriba Jah, Privateer Space, Inc., United States;

    • Rapporteur: Prof. Linli Guo, China Academy of Space Technology (CAST), China;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    2

    15:15

    Mixed-Integer GA optimization for the control of a formation of small satellites equipped with multi-constrained electric thrusters

    10

    confirmed

    Prof. Giovanni B. Palmerini

    Sapienza University of Rome

    Italy

    3

    15:25

    Tether-aided Formation Keeping for Multipoint Scientific Measurements in LEO

    10

    confirmed

    Mr. Basel Omran

    Skolkovo Institute of Science and Technology

    Russian Federation

    4

    15:35

    Segmentation-Driven 6D Pose Estimation of Spacecraft for Vision-based Relative Navigation in Space

    10

    confirmed

    Mr. Karl Martin Kajak

    DLR (German Aerospace Center)

    Germany

    5

    15:45

    Design of natural collision-free trajectories for the mission extension phase of a remote sensing formation flying mission

    10

    confirmed

    Ms. Francesca Scala

    Politecnico di Milano

    Italy

    6

    15:55

    Combined control and navigation approach to the robotic capture of space vehicles

    10

    confirmed

    Dr. Zeno Pavanello

    University of Padova, DII / CISAS – “G. Colombo”

    Italy

    7

    16:05

    Bearing-only navigation for proximity operations on cis-lunar non-keplerian orbits

    10

    confirmed

    Mr. Michele Ceresoli

    Politecnico di Milano

    Italy

    12

    16:15

    Formation flying control of the relative trajectory shape and size using Lorenz forces

    10

    confirmed

    Dr. Danil Ivanov

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    13

    16:25

    An Overview of Autonomous Optical Navigation for Deep-Space CubeSats

    10

    confirmed

    Ms. Eleonora Andreis

    Politecnico di Milano

    Italy

    14

    16:35

    A New Guidance and Control Architecture for Orbit Docking via Feedback Linearization

    10

    confirmed

    Dr. Mauro Pontani

    Sapienza University of Rome

    Italy

    1001

    16:45

    Three Degree-of-Freedom Reflectivity Control Devices for Extremely High Precision Formation Control

    10

    withdrawn

    Dr. Ahmed Kiyoshi Sugihara El Maghraby

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    1008

    16:55

    Drag-free Control of Time-delay System for Formation Flight of B-DECIGO Spacecraft

    10

    withdrawn

    Dr. Toshio Kamiya

    NEC Corporation

    Japan

    1009

    17:05

    An Algebraic Approach for the Motion Estimation of a Non-Cooperative Space Debris Target

    10

    confirmed

    Mr. Tetsuya Kusumoto

    The University of TOKYO, Graduate school

    Japan

    1010

    17:15

    Dual-quaternion based finite-time adaptive control for spacecraft autonomous proximity maneuver with pyramid-type constraints

    10

    confirmed

    Mrs. Liangyue Wang

    Harbin Institute of Technology

    China

    1011

    17:25

    a robust tasks-priority based coordinated control approach for spacecraft’s variable configuration formation flying

    10

    confirmed

    Mr. Xiaolong Wang

    Northwestern Polytechnical University

    China

    *

    Automated Guidance and Navigation for Rendezvous and Docking of Spacecraft using SDRE Controller and UKF estimator.

    confirmed

    Ms. Roshini Muralidhar

    India

    *

    Calibrated and Decalibrated Approximations of Satellite Relative Motion in a Restricted 3-Body Regime of Earth-Moon System

    Mr. Aniket Bire

    University of Arizona

    United States