págs. 1-7
A natural perturbation treatment of the Molniya orbital behavior,based on the TLE data set
págs. 73-75
Bringing in break-up events within a space objects catalogue
Alejandro Pastor, Jan Siminski, Guillermo Escribano, Manuel Sanjurjo Rivo , Diego Escobar
págs. 9-11
Efficient Numerical Solution of the Low-Thrust Lambert's problem
Lamberto Dell'Elce, Aaron J. Rosengren
págs. 12-14
Flyby dynamical characterisation with Jacobian eigenvalues
Alessandro Masat, Camilla Colombo, Arnaud Boutonnet
págs. 15-17
Semi-analytical propagation of NEO binaries: the history of the Janus mission targets 1991 VH and 1996 FG3
Oscar Fuentes Muñoz, Alex J. Meyer, Daniel J. Scheeres
págs. 18-20
Single-averaged analytical model for low-thrust collision avoidance manoeuvres
Juan Luis Gonzalo, Camilla Colombo
págs. 21-23
págs. 24-26
Statistical analysis of the long-term dynamical behavior of uncontrolled geostationary satellites near an unstable equilibrium point
Roberto Maurice Flores Le Roux , Mauro Pontani, Elena Fantino
págs. 29-31
Improving long-term special perturbations efficiency for low Earth orbits
Davide Amato, D. Vallado
págs. 32-34
Simultaneously quasi-critical and quasi-heliosynchronous orbits
R. Vilhena de Moraes, M. Lívia Galhego da Costa, A. F. B. A. Prado, J. P. S. Carvalho
págs. 35-37
Semi-analytical computation of center-stable and center-unstable manifolds in the geostationary belt
Miquel Barcelona, Alex Haro Provinciale , José María Mondelo González
págs. 38-40
Validation of GTDS and DSST Standalone versions against precise orbit ephemerides
Paul J. Cefola, Jacob Stratford, Rosario López Gómez , Juan Félix San Juan Díaz
págs. 41-43
págs. 44-46
págs. 49-51
A detailed dynamical model for inclination-only dependent lunisolar resonances. Effects on the ”eccentricity growth” mechanism
Edoardo Legnaro, Christos Efthymiopoulos
págs. 52-54
An Arnold diffusion mechanism for the Galileo satellites
Alexandre Pousse, Mar Giralt, Immaculada Baldomà Barraca , Marcel Guardia Munarriz
, Elissa Maria Alessi
págs. 55-58
Fourier Expansion of the J2 Potential as a prelude to Resonant Orbit Control Theory
Nadav Mailhot, Pini Gurfil
págs. 59-61
Lagrangian descriptors for global dynamics
Jérôme Daquin, Rémi Pédenon Orlanducci, Makrina Agaoglou, Guillermo García Sánchez, Ana María Mancho
págs. 62-64
Low energy interplanetary trajectories using multiple gravity assists
págs. 65-67
Lunar mean-motion and secular resonances
Aaron J. Rosengren, Di Wu, Lamberto Dell'Elce
págs. 68-70
Improving the Force Model of SGP4 using Neural Network
Hans Mauricio Carrillo Hernández, Edna Segura, Rosario López Gómez , Juan Félix San Juan Díaz
págs. 77-79
Apply the hybrid orbit propagators to the association problem in the GEO region
Juan Félix San Juan Díaz , Rosario López Gómez
, Carlos Yanez, Manuel Higueras Hernáez
págs. 80-82
Manoeuvre detection based on S3TSR data
Rafael Vázquez Valenzuela , Jose M. Montilla, Julio C. Sanchez, Jorge Galán Vioque
, Javier Rey Benayas, Jan Siminski
págs. 83-85
Analyzing transport phenomena in orbital conjunctions
págs. 87-89
Astrodynamical methods for collision avoidance automation
Jan Siminski, Klaus Merz, Volker Schaus
págs. 90-91
Automation of the collision risk management from conjunction data message reception up to the decision-making
Alexis Petit, Romain Lucken, Sacha Redel, Florent Deleflie , Vincent Morand, François Laporte
págs. 92-94
Covariance determination for uncertainty realism in collision probability estimates
Alejandro Cano, Alejandro Pastor, Eduardo Arias, Daniel Sáez, Joaquín Míguez, Manuel Sanjurjo Rivo , Diego Escobar
págs. 95-97
Deep learning for all-vs-all conjunction detection
Emma Stevenson, Víctor Rodríguez Fernández, Hodei Urrutxua Cereijo , David Camacho Fernández
págs. 98-100
Fast orbit propagation for conjunction screening
Ana S. Rivero, Claudio Bombardelli , Rafael Vázquez Valenzuela
págs. 101-103
A convex optimisation-based approach to detect and estimate manoeuvres
págs. 105-107
Assessment of uncertainty propagation techniques for the network embedding of the space resident population
Matteo Romano, Timoteo Carletti, Anne Lemaitre , Jérôme Daquin
págs. 108-110
Cislunar Space Domain Awareness: improved characterization and uncertainty quantification
Pablo Machuca, Aaron J. Rosengren
págs. 111-113
Combining Taylor polynomials and multifidelity dynamics for the efficient propagation of uncertainties in orbital mechanics
Alberto Fossà, Roberto Armellín , Emmanuel Delande
, Matteo Losacco, Francesco Sanfedino
págs. 114-116
Non-linear set propagation with generalised equinoctial orbital elements
Max I. Hallgarten La Casta, Luis Sánchez Fernandez Mellado, Davide Amato, Massimiliano Vasile
págs. 117-119
págs. 121-123
Preliminary analysis of an active debris removal mission for large constellations: a constraint programming methodology
Adrian Barea, Juan Luis Gonzalo, Camilla Colombo, Hodei Urrutxua Cereijo
págs. 124-126
Bhanu Kumar, Rodney L. Anderson, Rafael de la Llave Canosa
págs. 127-129
Shape-based low-thrust trajectory optimization enhanced via orthogonal functions, collocation and regularization
Sergio Cuevas del Valle, Hodei Urrutxua Cereijo , Pablo Solano López
págs. 130-132
Orbit Transfer using Theory of Functional Connections via change of variables
págs. 133-135
On optimal trajectories of solar sails
Alesia Herasimenka, Lamberto Dell'Elce, Jean Baptiste Caillau, Jean-Baptiste Pomet
págs. 136-138
Dynamical geometry associated with the collision manifold in the circular restricted three-body problem
Joshua Fitzgerald, Shane Ross
págs. 141-143
Canonical modeling of the Solar Radiation Pressure Perturbation
Nir Vegh, Vladimir Martinusi
págs. 144-146
CUDA implementation of the first derivative of the gravity potential
Carlos Rubio Sierra, Jesús Gonzalo de Grado , Jan Siminski, Alberto Escapa García
págs. 147-149
CUDAjectory: a GPU-based software for massive parallel orbit propagation
Adriano Filippo Inno, Camilla Colombo, Alessandro Masat, Paula Lorena Bucci, Florian Renk
págs. 150-152
Time integrator for second order in time problems
págs. 153-154
A curvilinear generalization of the Yamanaka-Ankersen state transition matrix
págs. 157-159
Influence of Apophis’ spin axis variations on a spacecraft during the 2029 close approach with Earth
S. Aljbaae, A. F. B. A. Prado, J. Souchay, Valerio Carruba
págs. 160-162
Formation design selection based on time and cost of reset
Davide Menzio, Ahmed Mahfouz , Florio Dalla Vedova, Holger Voos
págs. 163-165
págs. 166-168
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