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Implementation of a Pseudo-drag free system for the BepiColombo orbit determination at Mercury	15	withdrawn	Mr.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

session IPB

Paper title

Mode

Presentation status

Speaker

Affiliation

Country