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• W2052638050 abstract "No AccessSpecial Issue in Honor of Richard BattinInitial Relative Orbit Determination for Close-in Proximity OperationsDavid K. Geller and Alex PerezDavid K. GellerUtah State University, Logan, Utah 84322*Associate Professor, 4130 Old Main Hill. Associate Fellow AIAA.Search for more papers by this author and Alex PerezUtah State University, Logan, Utah 84322†Graduate Student, 4130 Old Main Hill.Search for more papers by this authorPublished Online:10 Mar 2015https://doi.org/10.2514/1.G000933SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Gauss C. F., Theoria Motus: Theory of the Motion of the Heavenly Bodies Moving About the Sun in Conic Sections, C. H. Davis Translation, Little Brown, Boston, 1857, pp. 161–234. Google Scholar[2] Battin R. H., An Introduction to the Mathematics and Methods of Astrodynamics, AIAA, New York, 1987, pp. 131–140. Google Scholar[3] Curtis H. D., Orbital Mechanics for Engineering Students, Elsevier, New York, 2005, pp. 236–245. Google Scholar[4] Clohessy W. H. and Wiltshire R., “Terminal Guidance System for Satellite Rendezvous,” Journal of the Aero/Space Sciences, Vol. 27, No. 9, 1960, pp. 653–658. doi:https://doi.org/10.2514/8.8704 LinkGoogle Scholar[5] Woffinden D. and Geller D., “Observability Criteria for Angles-Only Navigation,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 45, No. 3, 2009, pp. 1194–1208. doi:https://doi.org/10.1109/TAES.2009.5259193 IEARAX 0018-9251 CrossrefGoogle Scholar[6] Psiaki M., “Autonomous Orbit Determination for Two Spacecraft from Relative Position Measurements,” Journal of Guidance, Control, and Dynamics, Vol. 22, No. 2, 2007, pp. 305–312. doi:https://doi.org/10.2514/2.4379 JGCDDT 0162-3192 LinkGoogle Scholar[7] Li Q., Guo F., Zhou Y. and Jiang W., “Observability of Satellite to Satellite Passive Tracking from Angles Measurements,” IEEE International Conference on Control and Automation, ICCA 2007, IEEE, New York, 2007, pp. 1926–1931. doi:https://doi.org/10.1109/ICCA.2007.4376697 Google Scholar[8] Schmidt J., Geller D. and Chavez F. R., “Viability of Angles-Only Navigation for Orbital Rendezvous Operation,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2010-7755, 2010. doi:https://doi.org/10.2514/6.2010-7755 LinkGoogle Scholar[9] Gillis R. W. and Geller D. K., “Proximity Operations Using Low-Thrust Propulsion and Angles-Only Measurements in Geosynchronous Orbits,” Advances in the Astronautical Sciences, Vol. 141, 2011, pp. 549–562. ADASA9 0065-3438 Google Scholar[10] Chari R., Geller D., Norris H., DSouza C. and Brand T., “Autonomous Orbital Rendezvous Using Angles-Only Navigation,” AAS/AIAA Astrodynamics Specialists Conference, American Astronautical Soc. Paper 2001-497, 2001. Google Scholar[11] Woffinden D. C. and Geller K. D., “Relative Angles-Only Navigation and Pose Estimation for Autonomous Orbital Rendezvous,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 5, 2007, pp. 1455–1469. doi:https://doi.org/10.2514/1.28216 JGCDDT 0162-3192 LinkGoogle Scholar[12] Segal S., Carmi A. and Gurfil P., “Stereovision-Based Estimation of Relative Dynamics Between Non-Cooperative Satellites: Theory and Experiments,” IEEE Transactions on Control Systems Technology, Vol. 22, No. 2, 2014, pp. 568–584. doi:https://doi.org/10.1109/TCST.2013.2255288 IETTE2 1063-6536 CrossrefGoogle Scholar[13] Gaisas G., D’Amico S. and Ardeans J. S., “Angles-Only Navigation to a Noncooperative Satellite Using Relative Orbital Elements,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 2, 2014, pp. 439–451. doi:https://doi.org/10.2514/1.61494 JGCDDT 0162-3192 LinkGoogle Scholar[14] Klein I. and Geller D., “Zero Delta-V Solution to the Angles-Only Range Observability Problem During Orbital Proximity Operations,” Advances in Estimation, Navigation, and Spacecraft Control, edited by Choukroun D., Oshman Y., Thienel J. and Idan M.,Springer, Berlin, Heidelberg, 2015, pp. 351–369. doi:https://doi.org/10.1007/978-3-662-44785-7_19 Google Scholar[15] Geller D. K. and Klein I., “Angles-Only Navigation State Observability During Orbital Proximity Operations,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 6, 2014, pp. 1976–1983. doi:https://doi.org/10.2514/1.G000133 JGCDDT 0162-3192 LinkGoogle Scholar[16] Prussing J. E., Schneider A. M. and Timin M. E., “A Manual Method for Space Rendezvous Navigation and Guidance,” Journal of Spacecraft and Rockets, Vol. 6, No. 9, 1969, pp. 998–1006. doi:https://doi.org/10.2514/3.29746 JSCRAG 0022-4650 LinkGoogle Scholar Previous article Next article" @default.
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