Analytical and semi-analytical investigations of geosynchronous space debris with high area-to-mass ratios

Abstract This paper provides a Hamiltonian formulation of the averaged equations of motion with respect to short periods (1 day) of a space debris subjected to direct solar radiation pressure and orbiting near the geostationary ring. This theory is based on a semi-analytical theory of order 1 regarding the averaging process, formulated using canonical and non-singular elements for eccentricity and inclination. The analysis is based on an expansion in powers of the eccentricity and of the inclination, truncated at an arbitrary high order. First, the dynamical evolution of space debris released near the geostationary ring, with area-to-mass ratios as high as 40 m2/kg is analyzed within the framework of mid-term evolution (∼1 year) as well as long-term evolution (several decades). This study is carried out, using both simplified analytical models to clarify some properties, as well as our complete semi-analytical theory which leads to an accurate understanding of the mid-term and long-term evolution of the eccentricity and of the inclination. We also analyzed the coupling equations between the eccentricity and the inclination, considering a doubly averaged analytical model. Second, we also focused our attention on the comparison of various direct radiation pressure approximations in order to assess their consequences. Last, this paper claims to be the continuation and the counterpart of previous papers dealing with geosynchronous orbits and radiation pressure, that is Anselmo and Pardini (2005) [Anselmo, L., Pardini, C. Orbital evolution of geosynchronous objects with high area-to-mass ratios. In: Danesy, D. (Ed.), Proceedings of the Fourth European Conference on Space Debris, ESA SP-587. ESA Publications Division, Noordwijk, The Netherlands, pp. 279–284, 2005] and Valk et al. (submitted for publication) [Valk, S., Lemaitre, A., Deleflie, F. Semi-analytical theory of mean orbital motion for geosynchronous space debris under gravitational influence, Advances in Space Research, submitted for publication].

[1]  C. Chao,et al.  Applied Orbit Perturbation and Maintenance , 2005 .

[2]  Oliver Montenbruck,et al.  Satellite Orbits: Models, Methods and Applications , 2000 .

[3]  Pierre Exertier,et al.  Semi-analytical theory of the mean orbital motion. , 1995 .

[4]  Juan Getino,et al.  ORBITAL EVOLUTION OF HIGH-ALTITUDE BALLOON SATELLITES , 1997 .

[5]  J. Liou,et al.  Orbital Dynamics of High Area-To-Mass Ratio Debris and Their Distribution in the Geosynchronous Region , 2005 .

[6]  P. Farinella,et al.  Non-gravitational perturbations and satellite geodesy , 1987 .

[7]  A. Milani,et al.  Orbital perturbations due to radiation pressure for a spacecraft of complex shape , 1983 .

[8]  C. Pardini,et al.  Long-Term Evolution of High Earth Orbits: Effects of Direct Solar Radiation Pressure and Comparison of Trajectory Propagators , 2007 .

[9]  Thomas Schildknecht,et al.  Optical Observations of Space Debris in High-Altitude Orbits , 2005 .

[10]  Robert Bryant,et al.  THE EFFECT OF SOLAR RADIATION PRESSURE ON THE MOTION OF AN ARTIFICIAL SATELLITE , 1961 .

[11]  J. Henrard.  Virtual singularities in the artificial satellite theory , 1974 .

[12]  B. Agrawal.  Design of Geosynchronous Spacecraft , 1986 .

[13]  K. Aksnes,et al.  Short-period and long-period perturbations of a spherical satellite due to direct solar radiation , 1976 .

[14]  Chun C. Chao,et al.  On the propagation and control of geosynchronous orbits , 1983 .

[15]  C. Pardini,et al.  Orbital Evolution of Geosynchronous Objects with High Area-To-Mass Ratios , 2005 .

[16]  Florent Deleflie,et al.  Semi-analytical theory of mean orbital motion for geosynchronous space debris under gravitational influence , 2009 .

[17]  G. Beutler,et al.  Optical observations of space debris in GEO and in highly-eccentric orbits , 2002 .

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