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  • IAC-23
  • C1
  • IPB
  • session IPB

    Title

    Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM

    type

    interactive

    IPC members
    • Co-Chair: Dr. Diane Davis, National Aeronautics and Space Administration (NASA), Johnson Space Center, United States;

    • Co-Chair: Dr. Florian Renk, European Space Agency (ESA), Germany;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    Deployment of Lunar Orbital Station in High Circular Orbit: Alternative to NRHO

    15

    confirmed

    Mrs. Ekaterina Belyaeva

    Rocket Space Corporation Energia

    Russian Federation

    General Overview of Near-Earth Magnetic Anomaly Effects on Satellite Attitude Estimation

    15

    confirmed

    Dr. Demet Cilden-Guler

    Istanbul Technical University

    Türkiye

    MULTIDUAL QUATERNIONS BASED DYNAMICS MODELING FOR A RIGID-FLEXIBLE COUPLING SPACECRAFT AND APPLICATION

    15

    confirmed

    Prof. Daniel Condurache

    Technical University of Iasi

    Romania

    A constellation design for orbiting solar reflectors to enhance terrestrial solar energy

    15

    confirmed

    Dr. Onur Çelik

    University of Glasgow

    United Kingdom

    Boundary-Value Problem of Tisserand-Leveraging Transfers

    15

    confirmed

    Mr. Jin Cheng Hu

    Nanjing University of Aeronautics and Astronautics

    China

    mission to the trans-neptunian object sedna: a possible next step of humanity towards stars

    15

    confirmed

    Mr. Vladislav Zubko

    Space Research Institute (IKI), Russian Academy of Sciences (RAS)

    Russian Federation

    The capture of near-Earth asteroids in close proximity orbits with a two-spacecraft strategy using a linear approximation

    15

    confirmed

    Ms. Livia Ionescu

    University of Glasgow

    United Kingdom

    Dynamics and Control of Gyroscopic Stabilized Tether Satellite System in LEO

    15

    confirmed

    Mr. Stefano Aliberti

    Politecnico di Torino

    Italy

    Implementation of a Pseudo-drag free system for the BepiColombo orbit determination at Mercury

    15

    withdrawn

    Mr. Umberto De Filippis

    Sapienza University of Rome

    Italy

    New results on the mass-optimization analysis of a planetary sunshade system

    15

    confirmed

    Mr. Catello Leonardo Matonti

    Politecnico di Torino

    Italy

    study on short range formation flight and docking control using ac magnetic field

    15

    confirmed

    Mr. Hayate Tajima

    The University of TOKYO, Graduate school

    Japan

    Distributed Cooperative Spacecraft Surrounding Control with Input Saturation and Collision Avoidance

    15

    confirmed

    Prof. Yanning Guo

    Harbin Institute of Technology

    China

    Precise Orbit Determination (POD) with focus on physical accelerometer calibration of the geodetic satellites GRACE and GRACE-FO for thermospheric density assessment

    15

    withdrawn

    Dr. Florian Wöske

    ZARM, University of Bremen

    Germany

    Model Predictive Control with Sequential Convex Programming (SCP) for Cooperative/Non-cooperative Formation Flying Satellites

    15

    confirmed

    Dr. Sanjeeviraja Thangavel

    Singapore, Republic of

    Analysis of the effects of disturbing factors on the dynamics of a spacecraft in low-Earth orbit

    15

    confirmed

    Mr. Dmitrii Antsiferov

    Bauman Moscow State Technical University

    Russian Federation

    Methods for dynamic studies of close encounters and application to real cases

    15

    withdrawn

    Mr. Nicolo' Stronati

    Cranfield University

    United Kingdom

    Convex Optimization of Spacecraft Rest-to-Rest Attitude Reorientation Maneuvers with Keep-Out Constraints

    15

    confirmed

    Mr. Federico Gettatelli

    Sapienza University of Rome

    Italy

    attitude and vibration control of a flexible satellite using double-gimbal variable-speed control moment gyro with unbalanced rotor

    15

    Mr. Saumitra Barman

    Indian Institute of Technology Kharagpur

    India

    Optimal Steering Law for Single-Gimbal Control Moment Gyroscopes with Singularity Avoidance and Vibration Suppression

    15

    Dr. Zhili Hou

    Tsinghua University

    China

    An Analytical Approach for Constellation Low-Thrust Replenishment Exploiting J2 Effect

    15

    Dr. Simeng Huang

    China

    Observer-based fault-tolerant integrated orbit-attitude control of solar sail

    15

    confirmed

    Mr. Fuqiang Duan

    National University of Defense Technology

    China

    relative navigation problem for rendezvous of two non-cooperative nano-satellites

    15

    withdrawn

    Ms. Roberta Mancone

    Sapienza University of Rome

    Italy

    Developing an LQR/APF based Orbit correction, Orbit Prediction, and Navigation Control for CubeSat's Formation Flying

    15

    confirmed

    Dr. Sanjeeviraja Thangavel

    Singapore, Republic of

    model predictive control based on recurrent neural network for reusable launch vehicle with dynamics uncertainties

    15

    confirmed

    Ms. Qifan Liu

    Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics

    China

    Reaction wheels angular momentum management during interplanetary flight

    15

    confirmed

    Dr. Yaroslav Mashtakov

    Keldysh Institute of Applied Mathematics of RAS

    Russian Federation

    Two-impulse orbital transfer based on the solution of Lambert problem with optimal flight time

    15

    confirmed

    Mr. Vadim Kravchenko

    Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI

    Russian Federation

    Satellite Characterization Using the Theory of Functional Connections and Nelder-Mead Algorithm

    15

    confirmed

    Dr. Allan Kardec de Almeida Junior

    Instituto de Telecomunicações (Portugal)

    Portugal

    Attitude Control of an Earth-pointing Satellite Employing Novel Actuator Configurations for Global Asymptotic Stability

    15

    confirmed

    Mr. Anirudh Etagi

    India

    Path planning and control for asteroid ejecta collection after a kinetic impact

    15

    confirmed

    Mr. Giacomo Borelli

    Politecnico di Milano

    Italy

    Magnetorquers attitude control for formation flying in LEO

    15

    confirmed

    Ms. Uliana Monakhova

    Keldysh Institute of Applied Mathematics, RAS

    Russian Federation

    Satellite Routing with Quantum Annealing: Collecting Space Debris and On-orbit Servicing

    15

    confirmed

    Mr. Priyank Dubey

    University of Luxembourg

    Luxembourg

    Data-driven Online Optimization for Spacecraft Fuel Slosh

    15

    confirmed

    Dr. Omer Burak Iskender

    Nanyang Technological University

    Singapore, Republic of