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  • IAC-25
  • C1
  • IPB
  • session IPB

    Title

    Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM

    type

    interactive

    IPC members
    • Co-Chair: Dr. Vladimir Razoumny, RUDN University, Russian Federation;

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

    • Co-Chair: Prof. Manoranjan Sinha, Indian Institute of Technology Kharagpur, India;

    • Co-Chair: Dr. Feng Jinglang, University of Strathclyde, United Kingdom;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    high-resolution imaging in vleo: preliminary mission analysis and gnc design for the horus mission

    15

    confirmed

    Mr. Andrea Jimmy Pacursa

    Politecnico di Milano

    Italy

    A constrained task allocation-based algorithm for multi-satellite communication routing

    15

    confirmed

    Mr. Konstantinos Platanitis

    Cranfield University, UK

    United Kingdom

    Efficient low-thrust trajectory design using a multi-DNN framework

    15

    confirmed

    Dr. Ruida Xie

    Australia

    6-DOF Fuel-Optimal NRHO Rendezvous Trajectories with Time-Varying Illumination Constraints

    15

    confirmed

    Ms. Charlotte Bennett

    Purdue University

    United States

    Visual-Haptic Assisted Motion Planning for Precise Rendezvous and Docking of Satellites

    15

    confirmed

    Mr. Rakesh Kumar Sahoo

    Indian Institute of Technology Kharagpur

    India

    Engineering Excellence on Optical Head System Development: A leap for Lunar landings

    15

    confirmed

    Dr. Lee Spitler

    Macquarie University

    Australia

    Calibration and Precise Attitude Determination \\ Process for MUP Satellite

    15

    confirmed

    Mrs. Sirin Yakupoglu Altuntas

    TAI - Turkish Aerospace Industries, Inc

    Türkiye

    Design of elliptic orbit constellations for solar reflectors for terrestrial solar energy enhancement

    15

    confirmed

    Dr. Onur Çelik

    Delft University of Technology

    The Netherlands

    Mission design techniques for satellites operating in Low-Lunar Orbits

    confirmed

    Ms. Mathilda Bolis

    Politecnico di Milano

    Italy

    stochastic differential dynamic programming with polynomial chaos expansion for robust trajectory

    15

    confirmed

    Mr. Masato Shibukawa

    The Graduate Universty for Advanced Studies (SOKENDAI)

    Japan

    Map-Free Terrain Relative Navigation for the Moon, Mars, and Beyond

    15

    withdrawn

    Dr. John Christian

    Georgia Institute of Technology

    United States

    Passive stabilization using magnetorquers on a 1U student CubeSat

    15

    Mr. Simone Ceola

    Politecnico di Milano

    Italy

    Consistency Intelligence Control Method for Coordinated Pursuit of Non-Cooperative Targets in Multi-Spacecraft Systems

    15

    confirmed

    Dr. Suyi Liu

    Northwestern Polytechnical University;National Key Laboratory of Aerospace Flight Dynamics

    China

    An integrated framework for mission design and guidance for autonomous in-orbit servicing missions

    15

    confirmed

    Dr. Nathan Wallace

    The University of Sydney

    Australia

    Orbit Acquisition Methodology Using Differential Drag for CuBy Demonstrator - The Bavarian Cube Satellite Constellation for Bio-monitoring

    15

    Mr. Prachit Vijay Kamble

    S4 – Smart Small Satellite Systems GmbH

    Germany

    Precise control of satellite rendezvous and docking maneuver using physics-informed model predictive controller

    15

    confirmed

    Ms. Paridhi Choudhary

    Indian Institute of Technology Kharagpur

    India

    Contingency trajectory design for the launch-phase failure of cislunar missions

    15

    confirmed

    Dr. Zilong Chen

    Beihang University

    China

    Modelling and analysis of local toroidal coordinates for large-range quasi-periodic relative motion within mega constellation satellites

    15

    confirmed

    Dr. Yun Xu

    China

    An analytical framework for hybrid spiral-ellipse trajectories under atmospheric drag

    15

    confirmed

    Mr. Kenta Nakajima

    Kyushu University

    Japan

    Enhancing Robustness to Operational Contingencies in MEO Electric Orbit Raising through RAAN Management Strategy

    15

    confirmed

    Dr. David Morante

    Deimos Space SL

    Spain

    Spacecraft rendezvous and proximity operations using computer vision and SE(3) dynamics

    15

    confirmed

    Mr. Seur Gi Jo

    Embry-Riddle Aeronautical University

    United States

    Attitude control and sloshing suppression for complex fluid-filled spacecraft considering uncertainties

    15

    confirmed

    Prof. Bin Meng

    Beijing Institute of Control Engineering, Beijing, 100080, P.R. China

    China