Request a copy

Full Text

19

CITATIONS

19 Total citations

2 Recent citations

3.34 Field Citation Ratio

n/a Relative Citation Ratio

publications

0

supporting

0

mentioning

0

contrasting

0

Smart Citations

0

0

0

0

Citing PublicationsSupportingMentioningContrasting

View Citations

See how this article has been cited at scite.ai

scite shows how a scientific paper has been cited by providing the context of the citation, a classification describing whether it supports, mentions, or contrasts the cited claim, and a label indicating in which section the citation was made.

• Clohessy, W. H., and Wiltshire, R. S., "Terminal Guidance System for Satellite Rendezvous," Journal of the Aerospace Sciences, Vol.27, No.9, 1960, pp. 653-658.
• Lawden, D. F., "Optimal Trajectories for Space Navigation," Butterworth, London, 1963, pp. 79-86.
• Tschauner, J., and Hempel, P., "Optimale Beschleunigeungsprogramme für das Rendezvous-Manouever," Acta Astronautica, Vol.10, 1964, pp. 296-307.
• Tschauner, J., "The Elliptic Orbit Rendezvous," AIAA 4th Aerospace Sciences Meeting, AIAA Paper 66-537, Los Angeles, 27-29 June 1966
• Carter, T. E., "New Form for the Optimal Rendezvous Equations Near Keplerian Orbit," Journal of Guidance, Control, and Dynamics, Vol.13, No.1, 1990, pp. 183-186. doi:10.2514/3.20533
• Yamanaka, K., and Andersen, F., "New State Transition Matrix for Relative Motion on an Arbitrary Elliptical Orbit," Journal of Guidance, Control, and Dynamics, Vol.25, No.1, 2002, pp. 60-66. doi:10.2514/2.4875
• Alfriend. K. T., Vadali, S. R., Gurfil, P., How, J. P., and Breger, L. S., Spacecraft Formation Flying: Dynamics, Control, and Navigation, Elsevier, Oxford, 2009, Chap. 4, pp. 59-78.
• Gim, D.-W., and Alfriend, K. T., "State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit," Journal of Guidance, Control, and Dynamics, Vol.26, No.6, 2003, pp. 956-971. doi:10.2514/2.6924
• Gurfil, P., and Kasdin, N. J., "Nonlinear Modeling of Spacecraft Relative Motion in the Configuration Space," Journal of Guidance, Control, and Dynamics, Vol.27, No.1, 2004, pp. 154-157. doi:10.2514/1.9343
• Balaji, S. K., and Tatnall, A., "Precise Modeling of Relative Motion for Formation Flying Spacecraft," 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, 29 Sep.-3 Oct. 2003.
• Ketema, Y., "An Analytical Solution for Relative Motion with an Elliptic Reference Orbit," Journal of Astronautical Sciences, Vol.53, No.4, 2006, pp. 373-389.
• Lee, D., Cochran, J. E., and Jo, J. H., "Solutions to the Variational Equations for Relative Motion of Satellites," Journal of Guidance, Control, and Dynamics, Vol.30, No.3, 2007, pp. 671-678. doi:10.2514/1.24373
• Gurfil, P., and Kholshevnikov, K. V., "Manifolds and Metrics in the Relative Spacecraft Motion Problem," Journal of Guidance, Control, and Dynamics, Vol.29, No.4, July-Aug. 2006, pp. 1004-1010. doi:10.2514/1.15531
• Gronchi, G. F., "An Algebraic Method to Compute the Critical Points of the Distance Function Between Two Keplerian Orbits," Celestial Mechanics and Dynamical Astronomy, Vol.93, No.1, 2005, pp. 295-329. doi:10.1007/s10569- 005-1623-5
• Gronchi, G. F., "On the Uncertainty of the Minimal Distance Between Two Confocal Keplerian Orbits," Discrete and Continuous Dynamical Systems Series B, Vol.7, No.4, 2007, pp. 755-778.
• Condurache, D., and Martinusi, V., "Kepler's Problem in Rotating Reference Frames. Part 1: Prime Integrals. Vectorial Regularization," Journal of Guidance, Control, and Dynamics, Vol.30, No.1, 2007, pp. 192-200. doi:10.2514/1.20466
• Condurache, D., and Martinusi, V., "Kepler's Problem in Rotating Reference Frames. Part 2: Relative Orbital Motion," Journal of Guidance, Control, and Dynamics, Vol.30, No.1, 2007, pp. 201-213. doi:10.2514/1.20470
• Condurache, D., "New Symbolic Methods in the Study of Dynamic Systems," (in Romanian), Ph.D. Thesis, Gheorghe Asachi Technical Univ., Iasi, Romania, 1995.
• Condurache, D., and Martinusi, V., "Relative Spacecraft Motion in a Central Force Field," Journal of Guidance, Control, and Dynamics, Vol.30, No.3, 2007, pp. 873-876. doi:10.2514/1.26361
• Condurache, D., and Martinusi, V., "Foucault Pendulum-Like Problems: ATensorial Approach," International Journal of Nonlinear Mechanics, Vol.43, No.8, 2008, pp. 743-760. doi:10.1016/j.ijnonlinmec.2008.03.009.
• Condurache, D., and Martinusi, V., "Exact Solution to the Relative Orbital Motion in a Central Force Field," The 2nd International Symposium on Systems and Control in Aeronautics and Astronautics, Shenzhen, China, 10-12 Dec. 2008.
• Condurache, D., and Martinusi, V., "A Novel Hypercomplex Solution to Kepler's Problem," PADEU, Vol.19, Astronomy Department of the Eötvös University, Budapest, 2007, pp. 65-80.
• Condurache, D., and Martinusi,V., "Hypercomplex Eccentric Anomaly in the Unified Solution to the Relative Orbital Motion," AAS/AIAA Astrodynamics Specialist Conference, AAS Paper 09-321 Pittsburgh, PA, 9-13 Aug. 2009.
• Hamilton,W. R., "On Quaternions; or on a New System of Imaginaries in Algebra," The London, Edinburgh and Dublin Philosophical Magazine and Journal of Science, Series 3, Vol.35, 1844.
• Battin, R. H., An Introduction to the Mathematics and Methods of Astrodynamics, AIAA Education Series, 1999.
• Darboux, G., Leçons sur la Théorie Générale des Surfaces et les Applications Géometriques du Calcul Infinitesimal, Gauthier-Villars, Paris, 1887, Chap. 2.
• Fasano, A., and Marmi, S., Analytical Mechanics, Oxford Univ. Press, New York, 2006.
• Lurie, A. I., Analytical Mechanics, Springer, New York, 2002.
• Angeles, J., Fundamentals of Robotic Mechanical Systems: Theory, Methods, and Algorithms, Springer, New York, 2006.
• Bartels, R. E., "A Numerical Scheme for Ordinary Differential Equations Having Time Varying and Nonlinear Coefficients Based on the State Transition Matrix," NASATM-2002211776, 2002.
• Gantmaher, F. R., The Theory of Matrices, Chelsea, New York, 1959, Chap. 11.
• Condurache, D., and Martinusi, V., "Exact Solution to the Relative Orbital Motion in Eccentric Orbits," Solar System Research, Vol.43, No.1, 2009, pp. 41-52. doi:10.1134/S0038094609010043
• Condurache, D., and Martinusi,V., "TOChNOEREShENIEZADAChI OTNOSITEL'NOGO ORBITAL'NOGO DVIZhENIYa PO EKSTsENTRIChESKOI ORBITE," Astronomicheskii Vestnik/Astronomy Review, Vol.43, No.1, 2009, pp. 44-55.
• Condurache, D., and Martinusi,V., "AComplete Closed FormVectorial Solution to the Kepler Problem," Meccanica, Vol.42, No.5, 2007, pp. 465-476. doi:10.1007/s11012-007-9065-7