Author, Organisation |
Title |
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Pavel Trivailo, RMIT University
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KEYNOTE PRESENTATION: Enhancement of the Spacecraft Attitude Dynamics Capabilities via Combination of the Inertial Morphing and Reaction Wheels
[paper ] |
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Takayuki Hosonuma, The University of Tokyo
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TRICOM-1R Flight Dynamics Analysis: Angular Momentum Oscillation of Spinning Satellite in Highly Elliptical Orbit
[paper ] |
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Stéphanie Delavault, Centre National d'Etudes Spatiales
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Drag-Free and Attitude Control System in LEO using Cold Gas Propulsion System: a feedback from the MICROSCOPE mission
[paper ] |
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Hongyang Dong, Beihang University
|
Adaptive Attitude Tracking Control with Parameter Convergence in the Absence of Persistent Excitation
[paper ] |
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FORMATION FLYING & SATELLITE CONSTELLATIONS 1 - Chair: Pier Luigi Righetti
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Gabriella Gaias, Martin Lara, Camilla Colombo, Politecnico Di Milano
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Accurate Osculating/Mean Orbital Elements Conversions for Spaceborne Formation Flying
[paper ] |
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Alexey Grushevskii, Keldysh Institute of Applied Mathematics of RAS
|
Spatial Formation of High Inclined Orbits with Use of Gravity Assists
[paper ] |
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Ralph Kahle, German Aerospace Center DLR / GSOC
|
The Tandem-L Formation Flying Mission
[paper ] |
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Dirk Kuijper, CGI Deutschland Ltd. & Co. KG
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Sentinel-5P Loose Formation Flying with Suomi-NPP: LEOP, Orbit Acquisition and Orbit Maintenance
[paper ] |
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Zhen-Yu Li, National University of Defense Technology
|
Optimization of Multiple-Impulse Perturbed Cooperative Rendezvous for Spacecraft
[paper ] |
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Elena Fantino, Khalifa University of Science and Technology
|
Connecting Low-Energy Orbits in the Saturn system
[paper ] |
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Hirohisa Kojima, Tokyo Metropolitan University
|
Evaluation of Transition Performance to Jupiter Orbit using Electrodynamic Tether System
[paper ] |
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Ai Noumi, Japan Aerospace Exploration Agency
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On-Orbit Mass Property Estimation for Cargo Spacecraft using Operation Data by Machine Learning
[paper ] |
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Hélène Evain, Centre National d'Etudes Spatiales
|
Satellite Attitude Control with a Six-Control Moment Gyro cluster tested under Microgravity Conditions
[paper ] |
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Yue Wang, Beihang University
|
Dynamical Modeling of Coupled Orbit-Attitude Motion of a Rigid Body in the Gravity of an Asteroid Considered as a Polyhedron
[paper ] |
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Craig Watkins, Informative Technology Innovations
|
The Pioneer 10 Spin Anomaly as an Observation Artefact
[paper ] |
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FORMATION FLYING & SATELLITE CONSTELLATIONS 2 - Chair: Graham Dorrington
|
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Shuhei Matsushita, The University of Tokyo
|
Orbital design of formation flight to keep relative distance applied to space gravitational wave antenna B-DECIGO
[paper ] |
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Alexander Kharlan, Skolkovo Institute of Science and Technology
|
Deployment and Maintenance of Solar Sail-Equipped Cubesat Formation in LEO
[paper ] |
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Hao Zhang, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences
|
A Control Theoretical Analysis of Formation Flight with Inter-satellite Lorentz Forces
[paper ] |
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Sofya Spiridonova, Ralph Kahle, German Aerospace Center (DLR)
|
HRWS - An Ambitious 4+ Satellite Formation Flying Mission
[paper ] |
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Itziar Barat, Deimos @ ESA
|
Flex Tandem with Sentinel-3: Control Concept
[paper ] |
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Sung Wook Paek, Samsung SDI
|
Sun-synchronous repeat ground tracks and other useful orbits for future space missions
[paper ] |
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Brian Young, Jet Propulsion Laboratory / California Institute of Technology
|
Using Telemetry to Navigate the MarCO Cubesats to Mars
[paper ] |
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Martin Lara, University Of La Rioja
|
Design of quasi-satellite orbits: Analytical alternatives
[paper ] |
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Stefano Pessina, Eumetsat
|
Meteosat ranging antennas relocation: performance assessment and compensation using telescopes data service
[paper ] |
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Yang Yang, RMIT University
|
Consider Probability Hypothesis Density Filtering for Multiple Space Objects Tracking
[paper ] |
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Miguel Martin Serrano, Scisys
|
Aeolus Orbit Control Strategy: Analysis and Final Implementation
[paper ] |
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Gabriele Bellei, Deimos Space
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Navigation Challenges during ExoMars Trace Gas Orbiter Aerobraking Campaign
[paper ] |
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Anne Hickey, Sapienza University of Rome
|
Estimating atmospheric density profiles using orbit determination with a focus on JUICE and Cassini
[paper ] |
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Dongsuk Han, Jet Propulsion Laboratory / California Institute of Technology
|
Dawn’s final mission at Ceres: Navigation and Mission Design Experience
[paper ] |
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Dongsuk Han, Jet Propulsion Laboratory / California Institute of Technology
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Aerobraking the ExoMars TGO: The JPL Navigation Experience
[paper ] |
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Daniel Aguilar Taboada, Eumetsat
|
Sentinel-3 orbit control strategy
[paper ] |
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Hideyuki Tanno, Japan Aerospace Exploration Agency
|
Aeroheating test of re-entry capsule in Hypersonic High-Reynolds number flow
[paper ] |
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Matthew Rozek, RMIT University
|
Multi-Objective Optimisation of NRHO-LLO Orbit Transfer via Surrogate-Assisted Evolutionary Algorithms
[paper ] |
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Laurent Beauregard, ISAE-SUPAERO
|
Optimized transfers between Earth-Moon invariant manifolds
[paper ] |
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Boris Segret, ESEP - Paris Observatory
|
Optimizations of Autonomous Orbit Determination for a Deep-Space CubeSat
[paper ] |
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Tsutomu Ichikawa, Japan Aerospace Exploration Agency
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A Study of Orbit estimation for a Spacecraft by Using the Reduced order Filter
[paper ] |
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Petr Kuchynka, GMV INSYEN at ESA/ESOC
|
Uncertainties in GPS-based operational orbit determination of Copernicus Sentinel satellites
[paper ] |
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Zhen-Yu Li, National University of Defense Technology
|
Orbital Pursuit-Evasion Games with Incomplete Information in the Hill Reference Frame
[paper ] |
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Luyi Yang, National University of Defense Technology
|
Coplanar Maneuvers to Observe an Assigned Site Based on Satellite Viewing-Swath Geometry Analysis
[paper ] |
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Emmanuel Blazquez, ISAE-SUPAERO
|
Rendezvous Design in a Cislunar Near Rectilinear Halo Orbit
[paper ] |
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Irene Cavallari, Robin Petitdemange, ISAE-SUPAERO
|
Transfer from a Lunar Distant Retrograde Orbit to Mars through Lyapunov Orbits
[paper ] |
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Francesca Scala, Camilla Colombo, Ioannis Gkolias, Politecnico di Milano
|
Design of disposal orbits for high altitude spacecraft with a semi-analytical model
[paper ] |
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Changxuan Wen, Technology and Engineering Center for Space Utilization
|
Reachability Study for Spacecraft Maneuvering from a Distant Retrograde Orbit in the Earth-Moon System
[paper ] |
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Tomas Martin-Mur, Jet Propulsion Laboratory / California Institute of Technology
|
Navigating MarCO, the First Interplanetary CubeSats
[paper ] |
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Juan Manuel Garcia, GMV INSYEN at ESA/ESOC
|
Flying gyroless around Mars: a SW update for Mars Express
[paper ] |
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Yu Nakajima, Japan Aerospace Exploration Agency
|
Development of a GPS receiver for geosynchronous satellites toward autonomous operation
[paper ] |
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Javier Sanchez, GMV INSYEN at ESA/ESOC
|
Effect of the Air Drag Perturbation in the Eccentricity Vector for Very Low Earth Orbits
[paper ] |
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Yue Wang, Beihang University
|
Dynamical evolution analysis of standard geostationary transfer orbits injected by Chinese launchers
[paper ] |
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Klaas Vantounhout, CGI Deutschland Ltd. & Co. KG
|
A simple and efficient algorithm to search the Gaia Star Catalogue
[paper ] |
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Kate Ketdam, RMIT University
|
Australian Space Port for Small Satellites: Launch Concept
[paper ] |
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Klaus Merz, European Space Agency
|
Risk reduction and collision risk thresholds for missions operated at ESA
[paper ] |
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Tung-Han You, Mark Wallace, Jet Propulsion Laboratory / California Institute of Technology
|
Leveraging Mars Aerobraking Experience for the Venus Environment
[paper ] |
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Hiroshi Kato, Japan Aerospace Exploration Agency
|
Machine Learning for Atmospheric Drag Prediction of LEO satellites
[paper ] |
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F. Budnik, G. Bellei, F. Castellini, T. Morley, European Space Agency
|
BepiColombo: Flight Dynamics Operations during Launch and Early Orbit Phase
[paper ] |
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Robert Guilanyà Jané, GMV INSYEN at ESA/ESOC
|
ExoMars 2016 – Flight Dynamics commanding during the aerobraking operations for the Trace Gas Orbiter
[paper ] |
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Robert Guilanyà Jané, GMV INSYEN at ESA/ESOC
|
ExoMars 2016 – Flight Dynamics operations for targeting the Schiaparelli module EDL and the Trace Gas Orbiter Mars orbit insertion
[paper ] |
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Masahiro Nohmi, Shizuoka University
|
Past Results and Future Missions of STARS Series Satellite
[paper ] |
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Sung Wook Paek, Samsung SDI
|
Propagator for asteroid trajectories tool (PAT2) with educational purposes
[paper ] |
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Elisabet Canalias, Alain Lamy, Centre National d'Etudes Spatiales
|
Exploring the motion in libration point regions of perturbed three body problems - Application to orbits in the Mars-Phobos system
[paper ] |
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Juan Felix San Juan, University of La Rioja
|
Review of the Draper Semi-analytical Satellite Theory (DSST)
[paper ] |
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Paolo Izzo, Technion - Israel Institute of Technology
|
Periodic corrections in secular Milankovitch theory applied to passive debris removal
|
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Mirko Trisolini, Politecnico Di Milano
|
A density based approach to the propagation of re-entry uncertainties
[paper ] |
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Graham Dorrington, Pavel Trivailo, RMIT University
|
Utilizing the ‘Chaotic’ Tumbling of CubeSats
[paper ] |
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Tom Johnson, Dan Oltrogge, James Cooper, Analytical Graphics
|
Practical considerations and a realistic framework for a Space Traffic Management system
[paper ] |
||||
Craig Watkins, Informative Technology Innovations
|
Reconsideration of the Thermal Contribution to New Horizons Acceleration
[paper ] |
||||
Laurence Lorda, Centre National d'Etudes Spatiales
|
The Flight Dynamics Contribution to the Selection of MASCOT Landing Site on the Surface of the Asteroid Ryugu
[paper ] |
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Laurence Lorda, Centre National d'Etudes Spatiales
|
Flight Dynamics Analyses to reconstruct MASCOT’s trajectory on Ryugu’s surface
[paper ] |
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Antimo Damiano, RHEA Group
|
Flight Dynamics Analysis of extended Lifetime for the Metop-A GOME-2 Instrument
[paper ] |
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Pier Luigi Righetti, Eumetsat
|
Metop-C Deployment and Start of 3-Satellite Operations
[paper ] |
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Pier Luigi Righetti, Eumetsat
|
Avoidance of Radiofrequency Interferences with Metop-A and Metop-B during Metop-C early Operations
[paper ] |