IPB

session IPB

Title: Interactive Presentations - IAF ASTRODYNAMICS SYMPOSIUM
type: interactive
Date: 2022-09-19
Time: 12:50
Room: IP Area

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;
Co-Chair: Mr. David C. Folta, National Aeronautics and Space Administration (NASA), Goddard Space Flight Center, United States;
Co-Chair: Prof. Giovanni B. Palmerini, Sapienza University of Rome, Italy;
Co-Chair: Prof. Josep J. Masdemont, Universitat Politecnica de Catalunya (UPC), Spain;
Co-Chair: Prof. Jean de Lafontaine, NGC Aerospace Ltd., Canada;
Co-Chair: Prof. Othon Winter, UNESP - São Paulo Sate University, Brazil;
Co-Chair: Dr. Yuichi Tsuda, Japan Aerospace Exploration Agency (JAXA), Japan;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Space Domain Awareness for Cislunar Space: Parametrization and Characterization of Common Mission Scenarios	10		Dr. Pablo Machuca	University of California, San Diego	United States
Application and Analysis of Neural Networks for Unmodeled Dynamics in the Circular Restricted Three Body Problem	10	confirmed	Mr. Kyle Messick	Wichita State University	United States
Exploiting coherent patterns for the analysis of qualitative motion and the design of bounded orbits around small bodies	10	confirmed	Mr. Nicolò Bernardini	Surrey Space Centre - University of Surrey	United Kingdom
Direct Phasing Maneuver in Cis-Lunar Space: Sensitivity and Robustness analysis	10	confirmed	Ms. Catarina Antunes da Silva	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	France
Robust Design of Interplanetary Trajectories under Severe Uncertainty via Meta-Reinforcement Learning	10	confirmed	Mr. Lorenzo Federici	Sapienza University of Rome	Italy
IMPROVING ON-BOARD ATTITUDE KNOWLEDGE ACCURACY BY REAL-TIME LEARNING AND COMPENSATION OF MEASUREMENT ERRORS FOR HIGH ACCURACY SATELLITES	10	confirmed	Ms. Ritu Karidhal	Indian Space Research Organization (ISRO)	India
Nonlinear Observer and MPC-based algorithms for rendezvous maneuver with tumbling target	10	confirmed	Mr. Fabio Faliero	Politecnico di Torino	Italy
Spacecraft formation flying configuration design for space-based gravitational wave observatory	10	confirmed	Mr. Zhengxu Pan	National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an	China
Navigation analyses and trade-offs for the Martian moon exploration mission around Phobos	10		Mr. Edoardo Ciccarelli	University of Surrey	United Kingdom
Satellite attitude determination algorithms based only on star tracker measurements using TRIAD and q-method	10	confirmed	Dr. ELHASSEN BENFRIHA	Agence Spatiale Algérienne (ASAL)	Algeria
Design, development and analysis of Gear Based Variable Speed Control Moment Gyros	10	confirmed	Mr. Priyank Dubey	Indian Institute of Technology	India
Low-thrust control for IGSO satellite constellation using an improved convex optimization	10	confirmed	Dr. Sifeng Bi	University of Strathclyde / Mechanical and Aerospace Engineering	United Kingdom
Effects of Primary Shadowing on Asteroid Ejecta Captured into Periodic Orbits	10	confirmed	Ms. Anivid Pedros-Faura	University of Colorado Boulder	United States
On the orbit control of near repeat cycle orbits: the case of the BIOMASS mission	10	confirmed	Dr. Sérgio Brás	HE Space Operations	The Netherlands
Design Drivers of an Attitude Control System for Small CubeSats Using Magnetorquers	10	confirmed	Mr. Catalin-Daniel Neagu	Luleå University of Technology	Sweden
Multiple-shooting continuation of sun-assisted lunar transfers from the planar bicircular to the ephemeris model	10	confirmed	Dr. Sergey Trofimov	Keldysh Institute of Applied Mathematics, RAS	Russian Federation
Venus mission design leveraging low-energy capture and nonlinear orbit control	10	confirmed	Dr. Stefano Carletta	Sapienza University of Rome	Italy
Hardware-in-the-loop simulation framework for CubeSats proximity operations: application to the Milani mission	10	confirmed	Mr. Antonio Rizza	Politecnico di Milano	Italy
CubeSat attitude dynamics during flexible panels deployment	10	confirmed	Prof. Vladimir S. Aslanov	Samara National Research University (Samara University)	Russian Federation
Sensitivity analysis of asteroid ejecta models for future in-orbit sample collection mission	10	confirmed	Dr. Mirko Trisolini	Politecnico di Milano	Italy
To the Extended Rutherford’s formula and its application in the interplanetary mission design using multiple gravity assists	10	confirmed	Dr. Alexey Grushevskii	Keldysh Institute of Applied Mathematics of RAS	Russian Federation
Leveraging Maneuvers for Planetary Escape: strategy for a sample and return mission to Saturn	10		Mr. Federico Falorni	Politecnico di Milano	Italy
Coordination and Reactive Control of Multi-Spacecraft Formations for Earth Observation	10	confirmed	Mr. Claudio Vela	University of Naples "Federico II"	Italy
robust attitude control and observation system design for a flexible satellite with an immeasurable appendage	10	confirmed	Dr. Liming Fan	Beijing Institute of Spacecraft System Engineering, China Academy of Space Technology (CAST)	China
Resonant orbit for the expansion of achievable landing areas on the Venus surface in framework of Venera-D project	10	confirmed	Mr. Vladislav Zubko	Space Research Institute (IKI), Russian Academy of Sciences (RAS)	Russian Federation
Framework for Analyzing the Complex Interactions Between Spacecraft Motion and Slosh Dynamics in Low-G Environments	10	confirmed	Mr. William Elke	University of Minnesota Twin Cities	United States
SIX DOF ANALYSIS FOR ASTEROID AUTONOMOUS EXPLORATION	10	confirmed	Dr. Rodolfo Batista Negri	Federal University of São Paulo (UNIFESP)	Brazil
Deep learning based relative navigation about uncooperative space objects	10	confirmed	Mr. Massimo Piazza	Infinite Orbits	France
GNC of an cargo spacecraft on-orbit servicing Herschel at L2	10	confirmed	Mr. Ahmed Mahfouz	University of Luxembourg	Luxembourg
Psuedospectral Optimal Control of Spacecraft Rendezvous with Combined Differential Drag and Lorentz Forces	10		Dr. Mohamed Shouman	Toyota Technological Institute	Japan

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