Evolution of angular velocity for defunct satellites as a result of YORP: An initial study

Observations of defunct satellites show that these objects are generally rotating, with some having very fast rotation rates, yet the cause of these rapid rates is unknown. The observed secular change in the spin rate and spin axis orientation of asteroids is known to be caused by the Yarkovsky-O’Keefe-Radzievskii-Paddack (YORP) effect, however, its effect on inactive satellites in Earth orbit remains unexplored. This paper applies the YORP effect to defunct satellites and analyzes its effect on the spin rate and obliquity of these objects. This work uses two different satellite geometries to explore the secular change of the spin rate and obliquity caused by the YORP effect for inactive Geostationary Earth Orbit (GEO) satellites. One of the model satellites has an asymmetric geometry, which leads to the classical YORP effect as originally formulated for asteroids. The other model satellite is geometrically symmetric, but relies on mass distribution asymmetry to generate the YORP effect. For both models the secular change is explored with averaged dynamics, and the solutions of the averaged theory are compared with numerical integrations of the non-averaged equations of motion. Additionally, previously published observations of inactive GEO satellites are used to estimate the YORP torque acting on those bodies. A comparison between this torque and the expected torque on a defunct satellite shows that the two are of the same order of magnitude. These results motivate further study on the YORP effect in the realm of inactive satellites.

[1]  D. Vokrouhlický,et al.  Generalized YORP evolution: Onset of tumbling and new asymptotic states , 2007 .

[2]  M. Ziebart Generalized Analytical Solar Radiation Pressure Modeling Algorithm for Spacecraft of Complex Shape , 2004 .

[3]  D. Scheeres,et al.  Rotational dynamics of a solar system body under solar radiation torques , 2008 .

[4]  J. C. Van Der Ha,et al.  Long-term evolution of near-geostationary orbits , 1986 .

[5]  D. Rubincam,et al.  Radiative Spin-up and Spin-down of Small Asteroids , 2000 .

[6]  Maria Cecília Zanardi,et al.  Environmental torques acting on a low Earth orbiter cylindrical spacecraft , 2003 .

[7]  A. Fitzsimmons,et al.  The internal structure of asteroid (25143) Itokawa as revealed by detection of YORP spin-up , 2014 .

[8]  Colin R. McInnes,et al.  Solar Sailing: Technology, Dynamics and Mission Applications , 1999 .

[9]  David Vokrouhlický,et al.  YORP-induced long-term evolution of the spin state of small asteroids and meteoroids , 2002 .

[10]  Yu. N. Karavaev,et al.  Investigations of the evolution of optical characteristics and dynamics of proper rotation of uncontrolled geostationary artificial satellites , 2009 .

[11]  Moriba K. Jah,et al.  Coupled orbit–attitude motion of high area-to-mass ratio (HAMR) objects including efficient self-shadowing , 2014 .

[12]  Vaios Lappas,et al.  Long-Term Attitude Drift of Spinning Spacecraft Under Solar Radiation Torques , 2007 .

[13]  V. Modi,et al.  On the periodic solutions and resonance of spinning satellites in near-circular orbits , 1975 .

[14]  Anne Lemaitre,et al.  Semi-analytical investigations of high area-to-mass ratio geosynchronous space debris including Earth’s shadowing effects , 2008 .

[15]  D. Scheeres The dynamical evolution of uniformly rotating asteroids subject to YORP , 2006 .

[16]  D. Scheeres,et al.  New Solar Radiation Pressure Force Model for Navigation , 2010 .

[17]  Moriba K. Jah,et al.  Coupled orbit-attitude dynamics of high area-to-mass ratio (HAMR) objects: influence of solar radiation pressure, Earth’s shadow and the visibility in light curves , 2013, 1312.0067.

[18]  Nicholas L. Johnson,et al.  Space Debris Mitigation Guidelines , 2011 .

[19]  Holger Krag,et al.  Global Trends in Achieving Successful End-Of-Life Disposal in LEO and GEO , 2014 .

[20]  Y. Vigue,et al.  Improved Thermal Force Modeling for GPS Satellites , 1993 .

[21]  Petr Pravec,et al.  Direct Detection of the Asteroidal YORP Effect , 2007, Science.

[22]  D. Scheeres,et al.  Effect of density inhomogeneity on YORP: The case of Itokawa , 2008, 0805.2168.

[23]  Carmen Pardini,et al.  Space debris mitigation in geosynchronous orbit , 2006 .

[24]  A. Fitzsimmons,et al.  Spin Rate of Asteroid (54509) 2000 PH5 Increasing Due to the YORP Effect , 2007, Science.