SATELLITE REENTRY PREDICTIONS
PAPERS
Anselmo L., A. Cardillo, M.
Lucchesi, S. Trumpy, Il Decadimento Orbitale del
Cosmos 1402, Internal
Report C83-12, CNUCE Institute, CNR, Pisa, Italy, 7 July 1983.
Anselmo L., A. Cardillo, M.
Lucchesi, S. Trumpy, Orbital Decay of Cosmos 1402,
Internal Report C84-12, CNUCE
Institute, CNR, Pisa, Italy, 25 June 1984.
Anselmo L. and
S. Trumpy, Short-Term Predictions of Spacecraft Re-entry,
in Astrodynamics 1985, Proc. of the
AAS/AIAA Astrodynamics Specialist Conference held Aug. 12-15, 1985, Vail,
Colorado, Volume 58, Part I, Advances in the Astronautical Sciences series,
Univelt Inc., San Diego, California, Paper No. AAS 85-305, 1986, p. 134.
Anselmo L., Cosmos 1402 Re-entry Predictions: A
Retrospective Analysis, Proc.
Workshop on Re-entry of Space Debris, Darmstadt, FRG, 24-25 Sept. 1985 (ESA
SP-246, Feb. 1986), pp. 49-52.
Anselmo L. and
S. Trumpy, Short-Term Predictions of
Cosmos 1402 Reentry, The Journal of
the Astronautical Sciences, Vol. 34, No. 3, July-September 1986, pp.
271-285.
Anselmo L., A. Cardillo, A.
Foni, A. Santoro, S. Trumpy, Decadimento
Orbitale e Rientro nell’Atmosfera del Cosmos 1900, Internal Report C89-05, CNUCE Institute, CNR, Pisa, Italy, March
1989.
Anselmo L., Previsioni del Decadimento Orbitale del
Satellite SAX, Atti del X Congresso
Nazionale, Associazione Italiana Di Aeronautica ed Astronautica (AIDAA),
ETS Editrice, Pisa, Italy, March 1990, pp. 477-480.
Anselmo L., A. Cardillo, A.
Foni, A. Santoro, S. Trumpy, Il Rientro
del Satellite Cosmos 1900, Atti del X
Congresso Nazionale, Associazione Italiana Di Aeronautica ed Astronautica
(AIDAA), ETS Editrice, Pisa, Italy, March 1990, pp. 598-603.
Pardini C. e L. Anselmo, TDBM: Two-Dimension Ballistic Motion. Programma per
la simulazione del moto di un velivolo non propulso dotato di resistenza e
portanza in un’atmosfera planetaria, Internal Report C91-09, CNUCE Institute, CNR, Pisa, Italy, 29 May
1991.
Anselmo L., C.
Pardini, A. Santoro, S. Trumpy and P.E. Battaglia, Salyut-7/Kosmos-1686
Re-entry Predictions for the Italian Civil Defence Authority, in
The Reentry of Salyut-7/Kosmos-1686,
Proc. Int. Workshop on Salyut-7/Kosmos-1686 Reentry, ESOC, Darmstadt (D), 9
April 1991 (ESA SP-345, Aug. 1991) pp. 45-50.
Pardini C. e L. Anselmo, SATRAP: SATellite Reentry Analysis Program,
Internal Report C94-17, CNUCE Institute,
CNR,
Anselmo L., C.
Pardini, A. Rossi, Reentry predictions for Cosmos 398, FSW-1 5 and TSS-1R, Proc. of the
Second European Conference on
Space Debris, ESA/ESOC, Darmstadt (D), 17-19 March 1997 (ESA SP-393, May
1997), pp. 559-564.
Anselmo L., Il rientro incontrollato di satelliti
nell'atmosfera terrestre,
CNUCE/CNR, Pisa, Italy, 22 January 1999.
Pardini C. and L.
Anselmo, Reentry Predictions in Support of the IADC Test
Campaigns, Proc. of the
Third European Conference on Space
Debris, ESA/ESOC, Darmstadt (D), 19-21 March 2001 (ESA SP-473, Vol. 2,
October 2001), pp. 521-526.
Anselmo L. and C.
Pardini, The Management of the MIR Reentry in Italy,
Proc. of the International Workshop on
Mir Deorbit, ESA/ESOC, Darmstadt (D), 14 May 2001 (ESA SP-498, November
2002), pp. 83-90.
Pardini C. and L.
Anselmo, Performance Evaluation of Atmospheric Density Models for
Satellite Reentry Predictions with High Solar Activity Levels, Proceedings of the 23rd International
Symposium on Space Technology and Science, Matsue,
Pardini C. and
L. Anselmo, The Evolution of the Ballistic Parameter of the
BeppoSAX Satellite (2000-2002), ISTI Technical Report 2003-TR-21, ISTI/CNR,
Pisa, Italy, 28 January 2003.
Anselmo L., Risk Analysis and Management of the BeppoSAX
Reentry, ISTI Technical
Report 2003-TR-23, ISTI/CNR, Pisa, Italy, 5 March 2003.
Anselmo L. and
C. Pardini, BeppoSAX Reentry Campaign – Final Report,
ISTI Technical Report 2003-TR-24, ISTI/CNR,
Pardini C. and L.
Anselmo, On the Accuracy of Satellite Reentry Predictions,
Advances in Space Research, Vol. 34, No. 5, 2004, pp.
1038-1043, doi:10.1016/j.asr.2003.01.010.
Portelli C., L. Salotti, L. Anselmo, T. Lips, A. Tramutola, BEPPOSAX
Equatorial Uncontrolled Re-entry, Advances in Space Research,
Vol. 34, No. 5, 2004, pp. 1029-1037, 
doi:10.1016/j.asr.2003.11.011.
Anselmo
L. and C. Pardini, Computational Methods for Reentry Trajectories and Risk
Assessment, Advances in
Space Research, Vol. 35, No. 7,
2005, pp. 1343-1352, doi:10.1016/j.asr.2005.04.089.
Pardini C. and L.
Anselmo, Impact of the Time Span Selected
to Calibrate the Ballistic Parameter on Spacecraft Re-entry Predictions,
Advances in Space Research, Vol. 41, No. 7, 2008, pp. 1100-1114,
doi:10.1016/j.asr.2007.11.013.
Pardini C. and L.
Anselmo, USA-193 Decay Predictions with Public Domain Trajectory
Data and Assessment of the Post-Intercept Orbital Debris Cloud, Acta Astronautica, Vol. 64, Issues 7-8,
April-May 2009. pp. 787-795,
doi:10.1016/j.actaastro.2008.12.007.
Pardini C. and
L. Anselmo, Performances of Atmospheric Density Models during
Satellite Reentry Prediction Campaigns at Sunspot Minimum, Paper
presented at the 21st
International Symposium on Space Flight Dynamics, Toulouse, France, 28
September – 2 October 2009.
PRESENTATIONS
Pardini C., Servizio
Monitoraggio Oggetti Spaziali (SMOS), Seminar at CNUCE/CNR,
Pisa, 27 November 1998.
Pardini C. and L. Anselmo, Re-entry Predictions in Support of
the Inter-Agency Space Debris Co-ordination Committee Test Campaigns, Third European Conference on Space Debris,
ESA/ESOC,
Pardini
C., A Comparison of the Re-entry Predictions Using
Different Thermospheric Density Models During the 2002/#1 IADC Re-entry Test
Campaign, 20th
IADC Plenary Meeting, Guildford, Surrey, England, 9-12 April 2002.
Pardini
C. and L Anselmo, Performance Evaluation of
Atmospheric Density Models for Satellite Reentry Predictions with High Solar
Activity Levels, 23rd International Symposium on
Space Technology and Science, Matsue, Shimane Prefecture, Japan, May 26 – June
2, 2002.
Pardini
C. and L. Anselmo, On the Accuracy of
Satellite Reentry Predictions, 34th COSPAR Scientific Assembly,
The Second World Space Congress, Houston, TX, USA, 10-19 October 2002.
Anselmo L. and C. Pardini, Computational Methods for Reentry Trajectories, 35th COSPAR Scientific Assembly, Paris, France, 18-25
July 2004.
Pardini C. and L. Anselmo, Impact of the Time Span Selected
to Calibrate the Ballistic Parameter on Spacecraft Re-entry Predictions, 36th COSPAR Scientific Assembly,
Pardini C. and L. Anselmo, Re-entry Predictions for the Spacecraft COSMOS
1025, 25th IADC Plenary Meeting,
Anselmo L. and C. Pardini,
USA-193
Reentry Risk Assessment Using Unclassified Data Sources, 26th IADC Plenary Meeting, Moscow, 14-17
April 2008.
Pardini C. and L. Anselmo, USA-193 Decay Predictions
with Public Domain Trajectory Data and Assessment of the Post-Intercept Orbital
Debris Cloud, 59th International Astronautical Congress, Glasgow, Scotland, September 29 - October 3, 2008.
Anselmo L., E
se cade un satellite artificiale? La spazzatura che circonda la Terra. Il caso
del Cosmos 954 del 1978, Tunguska 1908: un asteroide colpisce
Pardini C. and L. Anselmo, Re-entry Predictions for
the Early Ammonia Servicer [EAS], ISTI/CNR Note,
Pardini C. and
L. Anselmo, Performances of Atmospheric Density Models
during Satellite Reentry Prediction Campaigns at Sunspot Minimum, 21st
International Symposium on Space Flight Dynamics, Toulouse, France, 28
September - 2 October 2009.
ATMOSPHERIC
DRAG MODELING
PAPERS
Anselmo L., Perturbazioni Orbitali Indotte dall’Atmosfera, Internal Report C85-09, CNUCE
Institute, CNR, Pisa, Italy, July 1985.
Pardini C., Calibrazione dei Modelli di Atmosfera di SATRAP per mezzo dello Studio del
Decadimento Orbitale di Satelliti Sferici e Cilindrici, Internal Report CNUCE
B4-1998-016, CNUCE Institute, CNR, Pisa, 16 November 1998.
Pardini
C. and L. Anselmo, Calibration of Semi-Empirical Atmosphere Models Through the Orbital
Decay of Spherical Satellites, in Astrodynamics 1999, Volume 103, Part II,
Advances in the Astronautical Sciences series, Univelt Inc., San Diego, California,
Paper AAS 99-384, 2000, pp. 1293-1305.
Pardini C. and L. Anselmo, Comparison of Thermospheric Density Models
by Satellite orbital Decay Analysis, 51st International Astronautical Congress, Rio de Janeiro, Brasil,
Paper IAF-00-A.5.01,
2-6 October, 2000.
Pardini C. and L. Anselmo, Comparison and Accuracy Assessment of
Semi-Empirical Atmosphere Models Through the Orbital Decay of Spherical
Satellites, The Journal
of the Astronautical Sciences, Vol. 49, No. 2, April-June 2001, pp.
255-268.
Pardini C., W. K. Tobiska and L. Anselmo, Pilot Service for
Improving Satellite Re-entry Predictions and Orbital Decay Modeling,
in ESA Space Weather Workshop: Space Weather
Applications Pilot Project, held on 16-18 December 2002 at ESA/ESTEC,
Noordwijk, The Netherlands, 2003.
Pardini C. and L. Anselmo, Performance Evaluation of
Atmospheric Density Models for Satellite Reentry Predictions with High Solar
Activity Levels, Transactions
of The Japan Society for Aeronautical and Space Sciences, Vol. 46, No. 151,
May 2003, pp. 42-46.
Pardini C., W. K. Tobiska and L. Anselmo, Analysis of the
Orbital Decay of Spherical Satellites Using Different Solar Flux Proxies and
Atmospheric Density Models, Advances
in Space Research, Vol. 37, No.
2, 2006, pp. 392-400, doi:10.1016/j.asr.2004.10.009.
Pardini C., L.
Anselmo, K. Moe and M. M. Moe, Drag and Energy Accommodation Coefficients During
Sunspot Maximum, Advances in Space Research (2009), doi:10.1016/j.asr.2009.08.034.
PRESENTATIONS
Pardini C. and L. Anselmo, Calibration of Semi-Empirical Atmosphere Models
Through the Orbital Decay of Spherical Satellites, AAS/AIAA Astrodynamics Specialist
Conference,
Pardini C. and L. Anselmo, Comparison of Thermospheric
Density Models by Satellite Orbital Decay Analysis, 51st International
Astronautical Congress, Rio de Janeiro, Brazil, 2-6 October 2000.
Pardini C., Accuracy
Assessment of Thermospheric Density Models, 19th IADC Plenary
Meeting, DLR, Cologne, Germany, 22-23 March 2001.
Pardini C., W. K. Tobiska and L. Anselmo, Pilot Service
for Improving Satellite Re-entry Predictions and Orbital Decay Modeling,
ESA Space Weather Workshop, Space Weather Applications Pilot Project, ESTEC,
Noordwijk, The Netherlands, 16-18 December 2002.
Pardini C., W. K. Tobiska and L.
Anselmo, Analysis
of the Orbital Decay of Spherical Satellites Using Different Solar Flux Proxies
and Atmospheric Density Models, 35th
COSPAR Scientific Assembly, Paris, France,
18-25 July 2004.
Pardini C., L.
Anselmo, K. Moe and M. M. Moe, Drag and Energy Accommodation Coefficients During
Sunspot Maximum, 37th
COSPAR Scientific Assembly, Montreal, Canada, 13-20 July 2008.
DRAG
MODELING APPLICATIONS
PAPERS
Pardini C. and L. Anselmo, Evolution of the Debris Cloud
Generated by the Fengyun-1C Fragmentation Event, Proceedings
of the 20th International Symposium on Space Flight Dynamics,
held in Annapolis (MD) on 24-28 September 2007 (NASA CP-2007-214158).
Pardini C. and L. Anselmo, Assessment of the Consequences of
the Fengyun-1C Breakup in Low Earth Orbit, Advances in Space Research, Vol. 44, No. 5, 2009, pp. 545-557, doi:10.1016/j.asr.2009.04.014.
Anselmo L. and C. Pardini, Analysis of the Consequences in
Low Earth Orbit of the Collision between Cosmos 2251 and Iridium 33,
Paper presented at the 21st International Symposium on Space Flight Dynamics,
Toulouse, France, 28 September – 2 October 2009.
PRESENTATIONS
Pardini C. and L. Anselmo,
Evolution of the Debris Cloud Generated by the
Fengyun-1C Fragmentation Event, 20th International Symposium on Space Flight Dynamics, Annapolis (MD),
24-28 September 2007.
Pardini C. and L. Anselmo, Assessment of the
Consequences of the Fengyun-1C Breakup in Low Earth Orbit, 37th
COSPAR Scientific Assembly,
Anselmo L. and C. Pardini, Analysis of the
Consequences in Low Earth orbit of the Collision between Cosmos 2251 and
Iridium 33, 21st International Symposium on Space Flight
Dynamics,
OTHER ORBITAL
PERTURBATIONS
PAPERS
Anselmo L., P. Farinella,
A. Milani and A.M. Nobili, Modelling of
Orbital Perturbations Due to Radiation Pressure for High Earth Satellites, Proc. Int. Symp. on Spacecraft Flight
Dynamics,
Anselmo L., B.
Bertotti, P. Farinella, A. Milani and A.M. Nobili, Orbital
Perturbations Due to Radiation Pressure for a Spacecraft of Complex Shape,
Celestial Mechanics, Vol. 29, 1983,
pp. 27-43.
Anselmo L., P.
Farinella, A. Milani and A.M. Nobili, Effects
of the Earth-Reflected Sunlight on the Orbit of the LAGEOS Satellite,
Astronomy
and Astrophysics, Vol. 117, 1983, pp. 3-8.
Anselmo L. and
P. Farinella, Alfven Drag for Satellites Orbiting in Jupiter’s
Plasmasphere, Icarus,
Vol. 58, 1984, pp. 182-185.
Ciufolini I.,
P. Farinella, A.M. Nobili, D. Lucchesi, L. Anselmo, Results of a Joint ASI-NASA Study on the LAGEOS Gravitomagnetic
Experiment and the Nodal Perturbations Due to Radiation Pressure and Particle
Drag Effects, Il Nuovo Cimento,
Vol. 108 B, No. 2, February 1993, pp. 151-162, doi: 10.1007/BF02874407.
Anselmo L. and
Pardini C., Orbital Evolution of Geosynchronous Objects with
High Area-to-Mass Ratios,
Proc. of the Fourth European Conference
on Space Debris, ESA/ESOC, Darmstadt (D), 18-20 April 2005 (ESA SP-587,
August 2005), pp. 279-284.
Pardini C. and
Anselmo L., Long-Term Evolution of
Geosynchronous Orbital Debris with High Area-to-Mass Ratios, Proceedings of the 25th
International Symposium on Space Technology and Science (Selected Papers),
Paper 2006-r-2-10, Japan Society for Aeronautical and Space Sciences and
Organizing Committee of the 25th ISTS, Kanazawa, Japan, 2006, pp.
1322-1327.
Pardini C. and
Anselmo L., Long-Term Evolution of Geosynchronous Orbital Debris
with High Area-to-Mass Ratios, ISTI Preprint 2007-PP-004, ISTI/CNR, Pisa, Italy, 5 March 2007.
Anselmo L. and
Pardini C., Long-Term Evolution of High Earth Orbits: Effects of
Direct Solar Radiation Pressure and Comparison of Trajectory Propagators,
ISTI Technical Report 2007-TR-008,
ISTI/CNR,
Pardini C. and
Anselmo L., Long-Term Evolution of Geosynchronous Orbital Debris
with High Area-to-Mass Ratios, Transactions of The
Valk S.,
Lemaître A. and Anselmo L., Analytical and Semi-Analytical
Investigations of Geosynchronous Space Debris with High Area-to-Mass Ratios, Advances in Space Research, Vol. 41, No. 7, 2008, pp. 1077-1090, doi: 10.1016/j.asr.2007.10.025.
Anselmo L. and
Pardini C., Dynamical
Evolution of High Area-to-Mass Ratio Debris Released into GPS Orbits, Advances in
Space Research, Vol. 43, No. 10,
2009, pp. 1491-1508, doi:
10.1016/j.asr.2009.01.017.
Anselmo, L. and Pardini, C., Long-Term Dynamical Evolution of High Area-to-Mass Ratio Debris Released into High
Earth Orbits, 3rd European Conference for
Aero-Space Sciences (EUCASS 2009), Versailles, France, July 6-9, 2009.
Anselmo L. and
Pardini C., Long-Term
Dynamical Evolution of
High Area-to-Mass Ratio Debris Released into High Earth Orbits, Acta
Astronautica, 2009, doi:10.1016/j.actaastro.2009.10.017.
PRESENTATIONS
Anselmo L. and
Pardini C., Dynamical
Evolution of High Area-to-Mass Ratio Debris Released into GPS Orbits, 37th
COSPAR Scientific Assembly, Montréal, Canada, July 13-20, 2008.
Anselmo, L. and Pardini, C., Long
Term Dynamical Evolution of High Area to Mass Ratio Debris Released into High
Earth Orbits, 3rd European Conference for
Aero-Space Sciences (EUCASS 2009), Versailles, France, July 6-9, 2009.