All Stories

  1. Reduction of Saturn Orbit Insertion Impulse Using Deep-Space Low Thrust

    Article • Journal of Guidance Control and Dynamics, April 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  2. Planetary exploration of Saturn moons Enceladus and Dione

    Article • Acta Astronautica, March 2020, Elsevier

    Prof. Jesus Pelaez

  3. Tether capture of spacecraft at Neptune

    Article • Acta Astronautica, March 2020, Elsevier

    Prof. Jesus Pelaez

  4. Minimum orbital intersection distance: an asymptotic approach

    Article • Astronomy and Astrophysics, December 2019, EDP Sciences

    Prof. Jesus Pelaez

  5. An efficient code to solve the Kepler equation

    Article • Astronomy and Astrophysics, November 2018, EDP Sciences

    Prof. Jesus Pelaez

  6. Comparative Saturn -Versus-Jupiter Tether Operation

    Article • Journal of Geophysical Research Space Physics, July 2018, American Geophysical Union (AGU)

    Prof. Jesus Pelaez

  7. On the minimum orbital intersection distance computation: a new effective method

    Article • Monthly Notices of the Royal Astronomical Society, June 2018, Oxford University Press (OUP)

    Prof. Jesus Pelaez

  8. An efficient code to solve the Kepler equation. Elliptic case.

    Article • Monthly Notices of the Royal Astronomical Society, January 2017, Oxford University Press (OUP)

    Prof. Jesus Pelaez

  9. New Analytic Solution with Continuous Thrust: Generalized Logarithmic Spirals

    Article • Journal of Guidance Control and Dynamics, October 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  10. Spiral Lambert’s Problem

    Article • Journal of Guidance Control and Dynamics, October 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  11. The theory of asynchronous relative motion II: universal and regular solutions

    Article • Celestial Mechanics and Dynamical Astronomy, September 2016, Springer Science + Business Media

    Prof. Jesus Pelaez, Prof. Daniel Condurache

  12. The theory of asynchronous relative motion I: time transformations and nonlinear corrections

    Article • Celestial Mechanics and Dynamical Astronomy, September 2016, Springer Science + Business Media

    Prof. Jesus Pelaez, Prof. Daniel Condurache

  13. Stability and chaos in Kustaanheimo–Stiefel space induced by the Hopf fibration

    Article • Monthly Notices of the Royal Astronomical Society, April 2016, Oxford University Press (OUP)

    Prof. Jesus Pelaez

  14. Temporarily Captured Asteroids as a Pathway to Affordable Asteroid Retrieval Missions

    Article • Journal of Guidance Control and Dynamics, November 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  15. Efficient Computation of Current Collection in Bare Electrodynamic Tethers in and beyond OML Regime

    Article • Journal of Aerospace Engineering, November 2015, American Society of Civil Engineers (ASCE)

    Prof. Jesus Pelaez

  16. Non-singular orbital elements for special perturbations in the two-body problem

    Article • Monthly Notices of the Royal Astronomical Society, October 2015, Oxford University Press (OUP)

    Prof. Jesus Pelaez

  17. DROMO propagator revisited

    Article • Celestial Mechanics and Dynamical Astronomy, September 2015, Springer Science + Business Media

    Prof. Jesus Pelaez

  18. Gravitational Actions upon Tethers in Nonuniform Gravity Fields with Revolution Symmetry

    Article • Journal of Guidance Control and Dynamics, August 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  19. Singularities in Dromo formulation. Analysis of deep flybys

    Article • Advances in Space Research, August 2015, Elsevier

    Prof. Jesus Pelaez

  20. Orbit propagation in Minkowskian geometry

    Article • Celestial Mechanics and Dynamical Astronomy, June 2015, Springer Science + Business Media

    Prof. Jesus Pelaez

  21. DROMO formulation for planar motions: solution to the Tsien problem

    Article • Celestial Mechanics and Dynamical Astronomy, March 2015, Springer Science + Business Media

    Prof. Jesus Pelaez

  22. Frozen-anomaly transformation for the elliptic rendezvous problem

    Article • Celestial Mechanics and Dynamical Astronomy, October 2014, Springer Science + Business Media

    Prof. Jesus Pelaez

  23. Jovian Capture of a Spacecraft with a Self-Balanced Electrodynamic Bare Tether

    Article • Journal of Spacecraft and Rockets, September 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  24. An asymptotic solution for the main problem

    Article • August 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  25. A New Regularization Method for Fast and Accurate Propagation of Roto-Translationally Coupled Asteroids

    Article • August 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  26. The ion beam shepherd: A new concept for asteroid deflection

    Article • Acta Astronautica, September 2013, Elsevier

    Prof. Jesus Pelaez

  27. GNC Design for Asteroid Orbit Modification Missions

    Article • August 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  28. A new set of integrals of motion to propagate the perturbed two-body problem

    Article • Celestial Mechanics and Dynamical Astronomy, March 2013, Springer Science + Business Media

    Prof. Jesus Pelaez

  29. Modifying the atlas of low lunar orbits using inert tethers

    Article • Acta Astronautica, October 2012, Elsevier

    Prof. Jesus Pelaez

  30. Asymptotic Solution for the Low-Thrust Restricted Two-Body Problem

    Article • August 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  31. Adaptive scheme for accurate orbit propagation

    Article • Journal of Aerospace Engineering Sciences and Applications, April 2012, Associacao Aerospacial Brasileira

    Prof. Jesus Pelaez

  32. Dynamics of a Tethered Observatory at Jupiter

    Article • Journal of Guidance Control and Dynamics, January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  33. Periodic Orbits of a Hill-Tether Problem Originated from Collinear Points

    Article • Journal of Guidance Control and Dynamics, January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  34. Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects

    Article • Journal of Aerospace Engineering Sciences and Applications, January 2012, Associacao Aerospacial Brasileira

    Prof. Jesus Pelaez

  35. Ion Beam Shepherd for Asteroid Deflection

    Article • Journal of Guidance Control and Dynamics, July 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  36. Asymptotic solution for the two-body problem with constant tangential thrust acceleration

    Article • Celestial Mechanics and Dynamical Astronomy, June 2011, Springer Science + Business Media

    Prof. Jesus Pelaez

  37. Ion Beam Shepherd for Contactless Space Debris Removal

    Article • Journal of Guidance Control and Dynamics, May 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  38. Energy Analysis of Bare Electrodynamic Tethers

    Article • Journal of Propulsion and Power, January 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  39. Asymptotic Solution for the Current Profile of Passive Bare Electrodynamic Tethers

    Article • Journal of Propulsion and Power, November 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  40. On the stability of artificial equilibrium points in the circular restricted three-body problem

    Article • Celestial Mechanics and Dynamical Astronomy, October 2010, Springer Science + Business Media

    Prof. Jesus Pelaez

  41. Libration Control of Electrodynamic Tethers Using the Extended Time-Delayed Autosynchronization Method

    Article • Journal of Guidance Control and Dynamics, May 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  42. Three-Body Dynamics and Self-Powering of an Electrodynamic Tether in a Plasmasphere

    Article • Journal of Propulsion and Power, May 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  43. Io Exploration with Electrodynamic Tethers

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  44. On the Dynamics of a Tethered System Near the Collineal Libration Points

    Article • August 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  45. A special perturbation method in orbital dynamics

    Article • Celestial Mechanics and Dynamical Astronomy, December 2006, Springer Science + Business Media

    Prof. Jesus Pelaez

  46. Floating bare tether as upper atmosphere probe

    Article • Journal of Geophysical Research Atmospheres, November 2006, American Geophysical Union (AGU)

    Prof. Jesus Pelaez

  47. Generator Regime of Self-Balanced Electrodynamic Bare Tethers

    Article • Journal of Spacecraft and Rockets, November 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  48. Linear Stability Analysis of Electrodynamic Tethers

    Article • Journal of Guidance Control and Dynamics, September 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  49. Dynamic Stability of Electrodynamic Tethers in Inclined Elliptical Orbits

    Article • Journal of Guidance Control and Dynamics, July 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  50. Libration Control of Electrodynamic Tethers in Inclined Orbit

    Article • Journal of Guidance Control and Dynamics, March 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  51. Self Balanced Electrodynamic Tether

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  52. On the numerical continuation of periodic orbits

    Article • Astronomy and Astrophysics, June 2002, EDP Sciences

    Prof. Jesus Pelaez

  53. Influence of a small end mass on tether-mediated orbital injection

    Article • Journal of Guidance Control and Dynamics, November 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  54. Bare Tethers for Electrodynamic Spacecraft Propulsion

    Article • Journal of Spacecraft and Rockets, March 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jesus Pelaez

  55. On the dynamics of the deployment of a tether from an orbiter—Part II. Exponential deployment

    Article • Acta Astronautica, September 1995, Elsevier

    Prof. Jesus Pelaez

  56. On the dynamics of the deployment of a tether from an orbiter—I. Basic equations

    Article • Acta Astronautica, July 1995, Elsevier

    Prof. Jesus Pelaez

  57. TRANSPORT OF MICROSPHERES BY THE HUMAN OVIDUCT IN VITRO AND THE EFFECT OF TREATMENT WITH MEGESTROL ACETATE

    Article • Reproduction, November 1971, Bioscientifica

    Prof. Jesus Pelaez