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Mechanik
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The Elliptic Rendezvous Problem in Dromo Formulation (AAS 14-382)
EDromo: An Accurate Propagator for Elliptical Orbits in the Perturbed Two-Body Problem (AAS 14-227)
Long-Term Dynamics of Fast Rotating Tethers Around Planetary Satellites (AAS 14-449)
Accurate and Fast Orbit Propagation With a New Complete Set of Elements (AAS 13-491)
DROMO Propagator Revisited, H. Urrutxua (AAS 13-488)
Deep Resonant GPS-Dynamics Due to the Geopotential (AAS 11-239)
Averaging and Mission Design: The Paradigm of an Enceladus Orbiter (AAS 09-199)
On the Thrust Capability of Electrodynamic Tethers Working in Generator Mode (AAS 09-242)
Exploration of the Jupiter Plasma Torus With a Self-Powered Electrodynamic Tether (AAS 09-240)
Lunar Analytical Theory for Polar Orbits in a 50-Degree Zonal Model (AAS 09-157)
Jovian Capture of a Spacecraft with a Self-Balanced Electrodynamic Bare Tether (AAS 09-241)
On the Attitude Propagation of an Axisymmetric Satellite (AAS 08-137)
Simple Control Laws for Self-Balanced Electrodynamic Tethers (AAS 08-153)
Long-Term Behavior of a Mercury Orbiter Perturbed by the Elliptic Motion of the Sun (AAS 08-236)
A Permanent Tethered Observatory at Jupiter: Dynamical Analysis (AAS 07-190)
A Permanent Tethered Observatory at Jupiter: Dynamical Analysis (AAS 07-190)
Analytical Theory for Science Orbits Around Planetary Satellites (AAS 07-221)
Analytical Theory for Science Orbits Around Planetary Satellites (AAS 07-221)
On the Design of a Science Orbit About Europa (AAS 06-168)
A Special Perturbation Method in Orbital Dynamics (AAS 05-167)
Generator Regime of Self Balanced Electrodynamic Bare Tethers (AAS 05-205)
Damping in the Dynamic Stability of Deorbiting Bare Tethers (AAS 03-215)
Libration Control of Electrodynamic Tethers in Inclined Orbit (AAS 03-214)
Phase Space Structure for Three-Dimensional Motion Around Europa (AAS 03-233)
Dynamic Stability of a Bare Tether as a Deorbiting Device (AAS 02-200)
Almost Periodic Orbits Around the Geostationary Points (AAS 02-110)
Stability Bounds for Three-Dimensional Motion Close to Asteroids (AAS 02-108)
Periodic Solutions in Rigid Electrodynamic Tethers on Inclined Orbits (AAS 01-188)
Periodic Solutions in Rigid Electrodynamic Tethers on Inclined Orbits (AAS 01-188)
On the Dynamical Behavior of a Spacecraft Orbiting Elongated Celestial Bodies (AAS 01-155)
On the Dynamical Behavior of a Spacecraft Orbiting Elongated Celestial Bodies (AAS 01-155)
Damping in Rigid Electrodynamic Tethers on Inclined Orbits (AAS 01-190)
Damping in Rigid Electrodynamic Tethers on Inclined Orbits (AAS 01-190)
On Periodic Orbits Around Geostationary Positions (AAS 00-156)
A Two Bar Model for the Dynamics and Stability of Electrodynamic Tethers (AAS 00-188)
A New Kind of Dynamic Instability in Electrodynamic Tethers (AAS 00-190)
Slingshot Orbital Injection Revisited
On the Radial Oscillation of an Electrodynamic Tether
Dynamical, Electrical and Thermal Coupling in a New Class of Electrodynamic Tethered Satellites
Searching for Repeating Ground Track Orbits: A Systematic Approach
On the Deployment of an Electrodynamic Tether From an Elliptical Orbit
Strategies for Maximizing the Lifetime of the SEDSAT Satellite
Frozen Orbits for the Zonal Moon Potential
Stability of the Pendular Motion of a Tethered System in Elliptical Orbit