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Artykuły w czasopismach na temat "Orbit method"
Chen, Q., J. D. Meiss i I. C. Percival. "Orbit extension method for finding unstable orbits". Physica D: Nonlinear Phenomena 29, nr 1-2 (listopad 1987): 143–54. http://dx.doi.org/10.1016/0167-2789(87)90051-0.
Pełny tekst źródłaSong, Xu Min, Yong Chen i Qi Lin. "Orbit Plan Method for General Rendezvous Problems". Applied Mechanics and Materials 543-547 (marzec 2014): 1385–88. http://dx.doi.org/10.4028/www.scientific.net/amm.543-547.1385.
Pełny tekst źródłaWang, Qianxin, Chao Hu i Ya Mao. "Correction Method for the Observed Global Navigation Satellite System Ultra-Rapid Orbit Based on Dilution of Precision Values". Sensors 18, nr 11 (12.11.2018): 3900. http://dx.doi.org/10.3390/s18113900.
Pełny tekst źródłaZhang, Mingjie, Jiangang Yang, Wanfu Zhang i Qianlei Gu. "Orbit Decomposition Method for Rotordynamic Coefficients Identification of Annular Seals". Applied Sciences 11, nr 9 (7.05.2021): 4237. http://dx.doi.org/10.3390/app11094237.
Pełny tekst źródłaFeng, Jingjing, Qichang Zhang, Wei Wang i 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.
Pełny tekst źródłaYe, Fei, Yunbin Yuan, Bingfeng Tan, Zhiguo Deng i 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, nr 1 (29.12.2018): 46. http://dx.doi.org/10.3390/rs11010046.
Pełny tekst źródłaQin, Huang, Zhang, Wang, Yan, Xie, Cao i Wang. "Precise Orbit Determination for BeiDou GEO/IGSO Satellites during Orbit Maneuvering with Pseudo-Stochastic Pulses". Remote Sensing 11, nr 21 (4.11.2019): 2587. http://dx.doi.org/10.3390/rs11212587.
Pełny tekst źródłaOLDEMAN, BART E., ALAN R. CHAMPNEYS i BERND KRAUSKOPF. "HOMOCLINIC BRANCH SWITCHING: A NUMERICAL IMPLEMENTATION OF LIN'S METHOD". International Journal of Bifurcation and Chaos 13, nr 10 (październik 2003): 2977–99. http://dx.doi.org/10.1142/s0218127403008326.
Pełny tekst źródłaKong, Qiaoli, Fan Gao, Jinyun Guo, Litao Han, Linggang Zhang i Yi Shen. "Analysis of Precise Orbit Predictions for a Hy-2A Satellite with Three Atmospheric Density Models Based on Dynamic Method". Remote Sensing 11, nr 1 (27.12.2018): 40. http://dx.doi.org/10.3390/rs11010040.
Pełny tekst źródłaLu, Qiuying, i Vincent Naudot. "Bifurcation Complexity from Orbit-Flip Homoclinic Orbit of Weak Type". International Journal of Bifurcation and Chaos 26, nr 04 (kwiecień 2016): 1650059. http://dx.doi.org/10.1142/s0218127416500590.
Pełny tekst źródłaRozprawy doktorskie na temat "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.
Pełny tekst źródłaLitsgård, 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.
Pełny tekst źródłaStevens, 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.
Pełny tekst źródłaThesis 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.
Znajdź pełny tekst źródłaElvidge, Michael Edward Carleton University Dissertation Engineering Mechanical and Aerospace. "A stochastic method for calculating spacecraft vulnerability to low earth orbit debris". Ottawa, 1994.
Znajdź pełny tekst źródłaHart, 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.
Pełny tekst źródłaSheng, 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.
Pełny tekst źródłaThis 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.
Pełny tekst źródłaVan, 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.
Pełny tekst źródłaIncludes 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.
Pełny tekst źródłaKsiążki na temat "Orbit method"
Duflo, M., M. Vergne i 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.
Pełny tekst źródłaNational Science Foundation (U.S.), red. Single orbit dynamics. Providence, RI: American Mathematical Society, 2000.
Znajdź pełny tekst źródłaDuval, Christian, Valentin Ovsienko i Laurent Guieu, red. The Orbit Method in Geometry and Physics. Boston, MA: Birkhäuser Boston, 2003. http://dx.doi.org/10.1007/978-1-4612-0029-1.
Pełny tekst źródłaGutzwiller, M. C. The motion of the moon as computed by the method of Hill, Brown, and Eckert. Washington: G.P.O., 1986.
Znajdź pełny tekst źródłaSincarsin, G. B. Geostationary orbital estimation using a Kalman filter. Downsview, Ont: Institute for Aerospace Studies, 1986.
Znajdź pełny tekst źródłaMatching of orbital integrals on GL(4) and GSp(2). Providence, R.I: American Mathematical Society, 1999.
Znajdź pełny tekst źródłaSmith, 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.
Znajdź pełny tekst źródłaBabillot, Martine. Rigidité, groupe fondamental et dynamique. Paris: SMF, 2002.
Znajdź pełny tekst źródłaHypoelliptic laplacian and orbital integrals. Princeton, N.J: Princeton University Press, 2011.
Znajdź pełny tekst źródła1959-, McGovern William M., red. Nilpotent orbits in semisimple Lie algebras. New York: Van Nostrand Reinhold, 1993.
Znajdź pełny tekst źródłaCzęści książek na temat "Orbit method"
Fujiwara, Hidenori, i Jean Ludwig. "Orbit Method". W Springer Monographs in Mathematics, 117–66. Tokyo: Springer Japan, 2014. http://dx.doi.org/10.1007/978-4-431-55288-8_5.
Pełny tekst źródłaZhang, Yasheng, Yanli Xu i Haijun Zhou. "Theory and Design Method of Hovering Orbit". W 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.
Pełny tekst źródłaZhang, Yasheng, Yanli Xu i Haijun Zhou. "Theory and Design Method of Responsive Orbit". W 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.
Pełny tekst źródłaKirillov, A. "The orbit method for nilpotent Lie groups". W Graduate Studies in Mathematics, 71–108. Providence, Rhode Island: American Mathematical Society, 2004. http://dx.doi.org/10.1090/gsm/064/03.
Pełny tekst źródłaRumberger, Matthias, i Jürgen Scheurle. "The Orbit Space Method: Theory and Application". W 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.
Pełny tekst źródłaCorwin, Lawrence. "Towards Harmonic Analysis on Homogeneous Spaces of Nilpotent Lie Groups". W 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.
Pełny tekst źródłaTorasso, Pierre. "The Poisson-Plancherel Formula for a Quasi-Algebraic Group with Abelian Radical and Reductive Generic Stabilizer". W 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.
Pełny tekst źródłaFujiwara, Hidénori. "Représentations Monomiales des Groupes de Lie Résolubles Exponentiels". W 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.
Pełny tekst źródłaPukanszky, L. "On a Property of the Quantization Map for the Coadjoint Orbits of Connected Lie Groups". W 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.
Pełny tekst źródłaZhang, Yasheng, Yanli Xu i Haijun Zhou. "Theory and Design Method of Spiral Cruising Orbit". W 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.
Pełny tekst źródłaStreszczenia konferencji na temat "Orbit method"
Friedman, Aharon, i Eva Bozoki. "Eigenvector method for optimized orbit correction". W Orbit correction and analysis in circular accelerators. AIP, 1994. http://dx.doi.org/10.1063/1.46769.
Pełny tekst źródłaTang, Y. N., i S. Krinsky. "Use of regularization method in the determination of ring parameters and orbit correction". W Orbit correction and analysis in circular accelerators. AIP, 1994. http://dx.doi.org/10.1063/1.46776.
Pełny tekst źródłaDu, Dongmei, i Qing He. "Orbit Shape Automatic Recognition Based on Artificial Neural Network". W ASME 2005 Power Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/pwr2005-50208.
Pełny tekst źródłaLi, Xiao-Jie, Yong Huang, Rui Guo, Ran-Ran Su i Kui Geng. "A new dynamic orbit determination method for GEO satellite after orbit maneuver". W 2015 International Conference on Mechanics and Mechatronics (ICMM2015). WORLD SCIENTIFIC, 2015. http://dx.doi.org/10.1142/9789814699143_0105.
Pełny tekst źródłaWalsh, Matthew T., i Mason A. Peck. "A Method for General Autonomous Orbit Matching". W 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.
Pełny tekst źródłaAshtari Larki, M. H., M. Maboodi i H. Bolandi. "Satellite orbit determination based on gradient method". W 2012 24th Chinese Control and Decision Conference (CCDC). IEEE, 2012. http://dx.doi.org/10.1109/ccdc.2012.6244407.
Pełny tekst źródłaDu, Heng, Boren Du i Wei Wang. "Neighboring orbit satellite image data conjunction method". W Second International Conference on Image and Graphics, redaktor Wei Sui. SPIE, 2002. http://dx.doi.org/10.1117/12.477075.
Pełny tekst źródłaKECHICHIAN, JEAN. "An analytic method of orbit determination in near-circular orbit using horizon sensor data". W 28th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-473.
Pełny tekst źródłaAl-Zamel, Z., i B. F. Feeny. "Improved Estimations of Unstable Periodic Orbits Extracted From Chaotic Sets". W 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.
Pełny tekst źródłaJun, Shu, Xu Limin i Li Jianbing. "An orbit transfer method for spatial object tracking". W 2017 29th Chinese Control And Decision Conference (CCDC). IEEE, 2017. http://dx.doi.org/10.1109/ccdc.2017.7978659.
Pełny tekst źródłaRaporty organizacyjne na temat "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), luty 2005. http://dx.doi.org/10.2172/839921.
Pełny tekst źródłaChao, Y. C. Orbit Correction Methods - Basic Formulation, Current Applications at Jefferson Lab, and Future Possibilities. Office of Scientific and Technical Information (OSTI), grudzień 1999. http://dx.doi.org/10.2172/754649.
Pełny tekst źródłaZilberman, Mark. Methods to Test the “Dimming Effect” Produced by a Decrease in the Number of Photons Received from Receding Light Sources. Intellectual Archive, listopad 2020. http://dx.doi.org/10.32370/iaj.2437.
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