Accurate and Fast Orbit Propagation With a New Complete Set of Elements (AAS 13-491)
A New Approach on the Long Term Dynamics of NEO's under Yarkovsky Effect (AAS 11-440)
A New Kind of Dynamic Instability in Electrodynamic Tethers (AAS 00-190)
A Permanent Tethered Observatory at Jupiter: Dynamical Analysis (AAS 07-190)
A Permanent Tethered Observatory at Jupiter: Dynamical Analysis (AAS 07-190)
A Special Perturbation Method in Orbital Dynamics (AAS 05-167)
A Two Bar Model for the Dynamics and Stability of Electrodynamic Tethers (AAS 00-188)
Damping in Rigid Electrodynamic Tethers on Inclined Orbits (AAS 01-190)
DROMO Propagator Revisited, H. Urrutxua (AAS 13-488)
Dynamical, Electrical and Thermal Coupling in a New Class of Electrodynamic Tethered Satellites
Dynamic Stability of a Bare Tether as a Deorbiting Device (AAS 02-200)
Dynamic Stability of Electrodynamic Tethers in Inclined Elliptical Orbits (AAS 03-538)
Earth Delivery of a Small NEO with an Ion Beam Shepherd (AAS 12-127)
EDromo: An Accurate Propagator for Elliptical Orbits in the Perturbed Two-Body Problem (AAS 14-227)
Exploration of the Jupiter Plasma Torus With a Self-Powered Electrodynamic Tether (AAS 09-240)
Frozen Orbits for Scientific Missions Using Rotating Tethers (AAS 12-269)
Generator Regime of Self Balanced Electrodynamic Bare Tethers (AAS 05-205)
Jovian Capture of a Spacecraft with a Self-Balanced Electrodynamic Bare Tether (AAS 09-241)
Linear Stability Analysis of Flexible Electrodynamic Tethers (AAS 03-539)
Long-Term Dynamics of Fast Rotating Tethers Around Planetary Satellites (AAS 14-449)
Modal Analysis of the Stability of Periodic Solutions in Electrodynamic Tethers (AAS 01-405)
On the Attitude Propagation of an Axisymmetric Satellite (AAS 08-137)
On the Control of a Permanent Tethered Observatory at Jupiter (AAS 07-369)
On the Deployment of an Electrodynamic Tether From an Elliptical Orbit
On the Radial Oscillation of an Electrodynamic Tether
On the Thrust Capability of Electrodynamic Tethers Working in Generator Mode (AAS 09-242)
Periodic Solutions in Rigid Electrodynamic Tethers on Inclined Orbits (AAS 01-188)
Relative Dynamics and Control of an Ion Beam Shepherd Satellite (AAS 12-246)
Simple Control Laws for Self-Balanced Electrodynamic Tethers (AAS 08-153)
Slingshot Orbital Injection Revisited
Solution of Optimal Continuous Low-Thrust Transfer Using Lie Transforms (AAS 13-931)
The Elliptic Rendezvous Problem in Dromo Formulation (AAS 14-382)