Добірка наукової літератури з теми "Orbit method"
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Статті в журналах з теми "Orbit method"
Chen, Q., J. D. Meiss, and I. C. Percival. "Orbit extension method for finding unstable orbits." Physica D: Nonlinear Phenomena 29, no. 1-2 (November 1987): 143–54. http://dx.doi.org/10.1016/0167-2789(87)90051-0.
Повний текст джерелаSong, Xu Min, Yong Chen, and Qi Lin. "Orbit Plan Method for General Rendezvous Problems." Applied Mechanics and Materials 543-547 (March 2014): 1385–88. http://dx.doi.org/10.4028/www.scientific.net/amm.543-547.1385.
Повний текст джерелаWang, Qianxin, Chao Hu, and Ya Mao. "Correction Method for the Observed Global Navigation Satellite System Ultra-Rapid Orbit Based on Dilution of Precision Values." Sensors 18, no. 11 (November 12, 2018): 3900. http://dx.doi.org/10.3390/s18113900.
Повний текст джерелаZhang, Mingjie, Jiangang Yang, Wanfu Zhang, and Qianlei Gu. "Orbit Decomposition Method for Rotordynamic Coefficients Identification of Annular Seals." Applied Sciences 11, no. 9 (May 7, 2021): 4237. http://dx.doi.org/10.3390/app11094237.
Повний текст джерелаFeng, Jingjing, Qichang Zhang, Wei Wang, and Shuying Hao. "A New Approach of Asymmetric Homoclinic and Heteroclinic Orbits Construction in Several Typical Systems Based on the Undetermined Padé Approximation Method." Mathematical Problems in Engineering 2016 (2016): 1–10. http://dx.doi.org/10.1155/2016/8585290.
Повний текст джерелаYe, Fei, Yunbin Yuan, Bingfeng Tan, Zhiguo Deng, and Jikun Ou. "The Preliminary Results for Five-System Ultra-Rapid Precise Orbit Determination of the One-Step Method Based on the Double-Difference Observation Model." Remote Sensing 11, no. 1 (December 29, 2018): 46. http://dx.doi.org/10.3390/rs11010046.
Повний текст джерелаQin, Huang, Zhang, Wang, Yan, Xie, Cao, and Wang. "Precise Orbit Determination for BeiDou GEO/IGSO Satellites during Orbit Maneuvering with Pseudo-Stochastic Pulses." Remote Sensing 11, no. 21 (November 4, 2019): 2587. http://dx.doi.org/10.3390/rs11212587.
Повний текст джерелаOLDEMAN, BART E., ALAN R. CHAMPNEYS, and BERND KRAUSKOPF. "HOMOCLINIC BRANCH SWITCHING: A NUMERICAL IMPLEMENTATION OF LIN'S METHOD." International Journal of Bifurcation and Chaos 13, no. 10 (October 2003): 2977–99. http://dx.doi.org/10.1142/s0218127403008326.
Повний текст джерелаKong, Qiaoli, Fan Gao, Jinyun Guo, Litao Han, Linggang Zhang, and Yi Shen. "Analysis of Precise Orbit Predictions for a Hy-2A Satellite with Three Atmospheric Density Models Based on Dynamic Method." Remote Sensing 11, no. 1 (December 27, 2018): 40. http://dx.doi.org/10.3390/rs11010040.
Повний текст джерелаLu, Qiuying, and Vincent Naudot. "Bifurcation Complexity from Orbit-Flip Homoclinic Orbit of Weak Type." International Journal of Bifurcation and Chaos 26, no. 04 (April 2016): 1650059. http://dx.doi.org/10.1142/s0218127416500590.
Повний текст джерелаДисертації з теми "Orbit method"
Mohamed, Ben Hadj Rhouma. "On the continuation of periodic orbits /." free to MU campus, to others for purchase, 1999. http://wwwlib.umi.com/cr/mo/fullcit?p9953845.
Повний текст джерелаLitsgård, Malte. "The Orbit Method and Geometric Quantisation." Thesis, Uppsala universitet, Analys och sannolikhetsteori, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-351508.
Повний текст джерелаStevens, Robert E. "Design of optimal cyclers using solar sails." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://library.nps.navy.mil/uhtbin/hyperion-image/02Dec%5FStevens.pdf.
Повний текст джерелаThesis advisor(s): I. Michael Ross, Dennis Byrnes. Includes bibliographical references (p. 119-120). Also available online.
Koblick, Darin C. "Parallel high-precision orbit propagation using the modified Picard-Chebyshev method." California State University, Long Beach, 2013.
Знайти повний текст джерелаElvidge, Michael Edward Carleton University Dissertation Engineering Mechanical and Aerospace. "A stochastic method for calculating spacecraft vulnerability to low earth orbit debris." Ottawa, 1994.
Знайти повний текст джерелаHart, Andrew Markland Stanley. "Application of the homotopy continuation method to low-eccentricity preliminary orbit determination." Thesis, Massachusetts Institute of Technology, 1991. http://hdl.handle.net/1721.1/42500.
Повний текст джерелаSheng, Liu Dong. "A New Method for Refinning Orbit of CPS Satellite Using Phase Measurement." International Foundation for Telemetering, 1990. http://hdl.handle.net/10150/613778.
Повний текст джерелаThis paper developed a new method of refinning GPS satellite orbit using phase measurement without knowing the GPS codes. Because this approach have no connection with any particular physical model, avoiding introducing any dynamic error, this method make it possible to get high precision GPS satellite orbit. A simulation computation has been conducted and gave an encouraging result.
Scott, Karen Patricia 1964. "Radiometric calibration of on-orbit satellite sensors using an improved cross-calibration method." Diss., The University of Arizona, 1998. http://hdl.handle.net/10150/282831.
Повний текст джерелаVan, Beusekom Craig Joseph. "A new guidance method for a DeltaV and re-entry constrained orbit transfer problem." Thesis, Massachusetts Institute of Technology, 2005. http://hdl.handle.net/1721.1/46571.
Повний текст джерелаIncludes bibliographical references (p. 153-154).
This thesis proposes a spacecraft guidance system designed for a unique class of orbit transfer problems. It considers a vehicle that undertakes a maneuver with the objective of precisely flying through a point in space at a particular time. The spacecraft must automatically determine a transfer orbit that will take it from a circular, low-earth parking orbit to a velocity-unconstrained rendezvous with a Keplerian trajectory. A constraint exists that both the final transfer orbit and the ultimate paths of any additional stages must lead rapidly to atmospheric reentry, typically within one revolution. Constrained to a fixed [delta]V resulting from a two stage thrust profile, the spacecraft must execute a burn maneuver that can effectively dissipate energy to place it on a transfer orbit with previously unknown velocity requirements. Finally, the guidance strategy should be robust to the uncertainties typically encountered in real spacecraft orbit transfer problems. In order to meet these constraints, this thesis first develops new analytic analysis of the relationship between reentry, perigee, and [delta]V. Next, a framework is developed for selecting a favorable transfer orbit while considering the various hard and soft constraints in the problem. Following transfer orbit selection, a plane of maneuver is calculated that maximizes likelihood of first stage reentry. Then traditional guidance strategies are adapted to the problem and hypothetical spacecraft design to produce a closed loop guidance solution. Results are presented that demonstrate the effectiveness of the new method.
by Craig Joseph Van Beusekom.
S.M.
Bengtsson, Bernander Karl. "A Method for Detecting Resident Space Objects and Orbit Determination Based on Star Trackers and Image Analysis." Thesis, Uppsala universitet, Avdelningen för visuell information och interaktion, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-236873.
Повний текст джерелаКниги з теми "Orbit method"
Duflo, M., M. Vergne, and N. V. Pedersen. The Orbit Method in Representation Theory. Boston, MA: Birkhäuser Boston, 1990. http://dx.doi.org/10.1007/978-1-4612-4486-8.
Повний текст джерелаNational Science Foundation (U.S.), ed. Single orbit dynamics. Providence, RI: American Mathematical Society, 2000.
Знайти повний текст джерелаDuval, Christian, Valentin Ovsienko, and Laurent Guieu, eds. The Orbit Method in Geometry and Physics. Boston, MA: Birkhäuser Boston, 2003. http://dx.doi.org/10.1007/978-1-4612-0029-1.
Повний текст джерелаGutzwiller, M. C. The motion of the moon as computed by the method of Hill, Brown, and Eckert. Washington: G.P.O., 1986.
Знайти повний текст джерелаSincarsin, G. B. Geostationary orbital estimation using a Kalman filter. Downsview, Ont: Institute for Aerospace Studies, 1986.
Знайти повний текст джерелаMatching of orbital integrals on GL(4) and GSp(2). Providence, R.I: American Mathematical Society, 1999.
Знайти повний текст джерелаSmith, R. L. Study of a homotopy continuation method for early orbit determination with the tracking and data relay satellite system (TDRSS). [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаBabillot, Martine. Rigidité, groupe fondamental et dynamique. Paris: SMF, 2002.
Знайти повний текст джерелаHypoelliptic laplacian and orbital integrals. Princeton, N.J: Princeton University Press, 2011.
Знайти повний текст джерела1959-, McGovern William M., ed. Nilpotent orbits in semisimple Lie algebras. New York: Van Nostrand Reinhold, 1993.
Знайти повний текст джерелаЧастини книг з теми "Orbit method"
Fujiwara, Hidenori, and Jean Ludwig. "Orbit Method." In Springer Monographs in Mathematics, 117–66. Tokyo: Springer Japan, 2014. http://dx.doi.org/10.1007/978-4-431-55288-8_5.
Повний текст джерелаZhang, Yasheng, Yanli Xu, and Haijun Zhou. "Theory and Design Method of Hovering Orbit." In Theory and Design Methods of Special Space Orbits, 37–90. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2948-6_3.
Повний текст джерелаZhang, Yasheng, Yanli Xu, and Haijun Zhou. "Theory and Design Method of Responsive Orbit." In Theory and Design Methods of Special Space Orbits, 199–223. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2948-6_7.
Повний текст джерелаKirillov, A. "The orbit method for nilpotent Lie groups." In Graduate Studies in Mathematics, 71–108. Providence, Rhode Island: American Mathematical Society, 2004. http://dx.doi.org/10.1090/gsm/064/03.
Повний текст джерелаRumberger, Matthias, and Jürgen Scheurle. "The Orbit Space Method: Theory and Application." In Ergodic Theory, Analysis, and Efficient Simulation of Dynamical Systems, 649–89. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-642-56589-2_27.
Повний текст джерелаCorwin, Lawrence. "Towards Harmonic Analysis on Homogeneous Spaces of Nilpotent Lie Groups." In The Orbit Method in Representation Theory, 1–9. Boston, MA: Birkhäuser Boston, 1990. http://dx.doi.org/10.1007/978-1-4612-4486-8_1.
Повний текст джерелаTorasso, Pierre. "The Poisson-Plancherel Formula for a Quasi-Algebraic Group with Abelian Radical and Reductive Generic Stabilizer." In The Orbit Method in Representation Theory, 213–27. Boston, MA: Birkhäuser Boston, 1990. http://dx.doi.org/10.1007/978-1-4612-4486-8_10.
Повний текст джерелаFujiwara, Hidénori. "Représentations Monomiales des Groupes de Lie Résolubles Exponentiels." In The Orbit Method in Representation Theory, 61–84. Boston, MA: Birkhäuser Boston, 1990. http://dx.doi.org/10.1007/978-1-4612-4486-8_3.
Повний текст джерелаPukanszky, L. "On a Property of the Quantization Map for the Coadjoint Orbits of Connected Lie Groups." In The Orbit Method in Representation Theory, 187–211. Boston, MA: Birkhäuser Boston, 1990. http://dx.doi.org/10.1007/978-1-4612-4486-8_9.
Повний текст джерелаZhang, Yasheng, Yanli Xu, and Haijun Zhou. "Theory and Design Method of Spiral Cruising Orbit." In Theory and Design Methods of Special Space Orbits, 91–137. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2948-6_4.
Повний текст джерелаТези доповідей конференцій з теми "Orbit method"
Friedman, Aharon, and Eva Bozoki. "Eigenvector method for optimized orbit correction." In Orbit correction and analysis in circular accelerators. AIP, 1994. http://dx.doi.org/10.1063/1.46769.
Повний текст джерелаTang, Y. N., and S. Krinsky. "Use of regularization method in the determination of ring parameters and orbit correction." In Orbit correction and analysis in circular accelerators. AIP, 1994. http://dx.doi.org/10.1063/1.46776.
Повний текст джерелаDu, Dongmei, and Qing He. "Orbit Shape Automatic Recognition Based on Artificial Neural Network." In ASME 2005 Power Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/pwr2005-50208.
Повний текст джерелаLi, Xiao-Jie, Yong Huang, Rui Guo, Ran-Ran Su, and Kui Geng. "A new dynamic orbit determination method for GEO satellite after orbit maneuver." In 2015 International Conference on Mechanics and Mechatronics (ICMM2015). WORLD SCIENTIFIC, 2015. http://dx.doi.org/10.1142/9789814699143_0105.
Повний текст джерелаWalsh, Matthew T., and Mason A. Peck. "A Method for General Autonomous Orbit Matching." In 2018 AIAA Guidance, Navigation, and Control Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0870.
Повний текст джерелаAshtari Larki, M. H., M. Maboodi, and H. Bolandi. "Satellite orbit determination based on gradient method." In 2012 24th Chinese Control and Decision Conference (CCDC). IEEE, 2012. http://dx.doi.org/10.1109/ccdc.2012.6244407.
Повний текст джерелаDu, Heng, Boren Du, and Wei Wang. "Neighboring orbit satellite image data conjunction method." In Second International Conference on Image and Graphics, edited by Wei Sui. SPIE, 2002. http://dx.doi.org/10.1117/12.477075.
Повний текст джерелаKECHICHIAN, JEAN. "An analytic method of orbit determination in near-circular orbit using horizon sensor data." In 28th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-473.
Повний текст джерелаAl-Zamel, Z., and B. F. Feeny. "Improved Estimations of Unstable Periodic Orbits Extracted From Chaotic Sets." In ASME 2001 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/detc2001/vib-21585.
Повний текст джерелаJun, Shu, Xu Limin, and Li Jianbing. "An orbit transfer method for spatial object tracking." In 2017 29th Chinese Control And Decision Conference (CCDC). IEEE, 2017. http://dx.doi.org/10.1109/ccdc.2017.7978659.
Повний текст джерелаЗвіти організацій з теми "Orbit method"
Parker, B. Novel Method of Compensation of the Effects of Detector Solenoid on the Vertical Beam Orbit in a Linear Collider. Office of Scientific and Technical Information (OSTI), February 2005. http://dx.doi.org/10.2172/839921.
Повний текст джерелаChao, Y. C. Orbit Correction Methods - Basic Formulation, Current Applications at Jefferson Lab, and Future Possibilities. Office of Scientific and Technical Information (OSTI), December 1999. http://dx.doi.org/10.2172/754649.
Повний текст джерелаZilberman, Mark. Methods to Test the “Dimming Effect” Produced by a Decrease in the Number of Photons Received from Receding Light Sources. Intellectual Archive, November 2020. http://dx.doi.org/10.32370/iaj.2437.
Повний текст джерела