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- W1991738142 abstract "No AccessEngineering NoteAttitude Dynamics and Control of Drag-Balance CubeSatsFabio Santoni and Leonard FelicettiFabio SantoniDipartimento di Ingegneria Astronautica, Università degli Studi di Roma “La Sapienza”, 00138 Rome, Italy*Associate Professor, Dipartimento di Ingegneria Astronautica, Elettrica ed Energetica, Via Salaria 851.Search for more papers by this author and Leonard FelicettiDipartimento di Ingegneria Astronautica, Università degli Studi di Roma “La Sapienza”, 00138 Rome, Italy†Ph.D. Student, Dipartimento di Ingegneria Astronautica, Elettrica ed Energetica, Via Salaria 851.Search for more papers by this authorPublished Online:29 Oct 2013https://doi.org/10.2514/1.59638SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Yurasov V. S., Nazarenko A. I., Cefola P. J. and Alfriend K. T., “Results and Issues of Atmospheric Density Correction,” Journal of Astronautical Sciences, Vol. 52, No. 3, 2004, pp. 281–300. CrossrefGoogle Scholar[2] Sutton E. K., Nerem R. S. and Forbes J. M., “Densities and Winds in the Thermosphere Deduced from Accelerometer Data,” Journal of Spacecraft and Rockets, Vol. 44, No. 6, 2007, pp. 1210–1219. doi:https://doi.org/10.2514/1.28641 JSCRAG 0022-4650 LinkGoogle Scholar[3] Tapley B. D., Ries J., Bettadpur S. and Cheng M., “Neutral Density Measurements from the Gravity Recovery and Climate Experiment Accelerometers,” Journal of Spacecraft and Rockets, Vol. 44, No. 6, 2007, pp. 1220–1225. doi:https://doi.org/10.2514/1.28843 JSCRAG 0022-4650 LinkGoogle Scholar[4] Heidt H., Puig-Suari J., Moore A., Nakasuka S. and Twiggs R., “CubeSat: A New Generation of Picosatellite for Education and Industry Low-Cost Space Experimentation,” Proceedings of the 14th Annual AIAA/USU Small Satellite Conference, Paper SSC00-V-5, Utah State Univ., Logan, UT, Aug. 2000, pp. 21–24. Google Scholar[5] Jacchia L. G. and Verniani F., “Atmospheric Densities and Temperatures From the Drag Analysis of the San Marco Satellite,” Smithsonian Institution Astrophysical Lab., Smithsonian Astronomical Observatory Special Rept. 193, Cambridge, MA, Nov. 1965. Google Scholar[6] Broglio L., “Air Density Between 200 and 300 km Equatorial Obtained by San Marco I Satellite,” Space Research VII: Proceedings of the Seventh International Space Symposium, edited by Smith-Rose R. L., Bowhill S. A. and King J. W., Vienna, 1966, pp. 1135–1147. Google Scholar[7] Arduini C., Broglio L. and Ponzi U., “Drag-Balance Measurements in the San Marco D/L Mission,” Advances in Space Research, Vol. 13, No. 1, 1993, pp. 185–200. doi:https://doi.org/10.1016/0273-1177(93)90018-7 ASRSDW 0273-1177 CrossrefGoogle Scholar[8] Santoni F., Piergentili F. and Graziani F., “Broglio Drag-Balance for Neutral Thermosphere Density Measurement on UNICubeSAT,” Advances in Space Research, Vol. 45, No. 5, March 2010, pp. 651–660. doi:https://doi.org/10.1016/j.asr.2009.10.001 ASRSDW 0273-1177 CrossrefGoogle Scholar[9] Hughes P. C., Spacecraft Attitude Dynamics, Wiley, New York, 1986, pp. 97–100. Google Scholar[10] Reynolds R. and Creamer G., “Global Lyapunov Control of Spin Stabilized Spacecraft,” Proceedings of the 2001 Flight Mechanics Symposium, edited by Lynch J. P., NASA CP—2001-209986, June 2001, pp. 285–293. Google Scholar[11] Stickler A. C. and Alfriend K. T., “Elementary Magnetic Attitude Control System,” Journal of Spacecraft and Rockets, Vol. 13, No. 5, 1976, pp. 282–287. doi:https://doi.org/10.2514/3.57089 JSCRAG 0022-4650 LinkGoogle Scholar[12] Pal P. K. and Selby V. H., “Magnetic Attitude Control System for Spinning Small Spacecraft,” Proceedings of the AIAA/USU Conference on Small Satellites Attitude Control I, SSC90-VII-3, Utah State Univ., 1990. Google Scholar[13] Santoni F. and Tortora P., “Magnetic Attitude Determination and Control of Small Spinning Spacecraft,” AIAA/AAS Astrodynamics Specialist Conference, AIAA Paper 2000-4350, Aug. 2000. LinkGoogle Scholar Previous article Next article" @default.
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