標(biāo)題: Titlebook: Dynamics of Satellites (1969); Proceedings of a Sym Bruno Morando (Docteur ès Sciences) Conference proceedings 1970 Springer Verlag, Berlin [打印本頁] 作者: 惡夢(mèng) 時(shí)間: 2025-3-21 19:24
書目名稱Dynamics of Satellites (1969)影響因子(影響力)
書目名稱Dynamics of Satellites (1969)影響因子(影響力)學(xué)科排名
書目名稱Dynamics of Satellites (1969)網(wǎng)絡(luò)公開度
書目名稱Dynamics of Satellites (1969)網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Dynamics of Satellites (1969)被引頻次
書目名稱Dynamics of Satellites (1969)被引頻次學(xué)科排名
書目名稱Dynamics of Satellites (1969)年度引用
書目名稱Dynamics of Satellites (1969)年度引用學(xué)科排名
書目名稱Dynamics of Satellites (1969)讀者反饋
書目名稱Dynamics of Satellites (1969)讀者反饋學(xué)科排名
作者: 委托 時(shí)間: 2025-3-21 20:44
ndness and efficiency of their welcome. The interpreters who translated with virtuosity during the whole symposium also deserve our gratitude. I am grateful also for the care and skill with which Springer-Verlag has printed this volume.978-3-642-99968-0978-3-642-99966-6作者: 結(jié)束 時(shí)間: 2025-3-22 02:36
Gespr?chskompetenz digitaler Agentenperiods are about 57 days and 68 days. These values diminish with increasing eccentricity. It is convenient to note the greater stability of retrograde satellites..The effect of solar radiation pressure is obviously more intensive than in the case of satellites of the Earth. The resonance condition 作者: abject 時(shí)間: 2025-3-22 05:24
,Ausgew?hlte Konstruktionstheorieen, a discussion of the estimated accuracy of these new determinations is given. The potential accuracy of these results is shown to be about an order of magnitude better than the presently quoted error bounds.作者: Largess 時(shí)間: 2025-3-22 12:48 作者: anchor 時(shí)間: 2025-3-22 16:13 作者: anchor 時(shí)間: 2025-3-22 19:38
https://doi.org/10.1007/3-540-30724-9he simulated data, and with previous analytic results from the actual data on Cosmos 41..Extensive data from many resonant 12 and 24 h satellites is currently being processed by the mean element program. Preliminary determinations from this data are given. The final result should be definitive infor作者: LAPSE 時(shí)間: 2025-3-23 00:09
A Short Study on the Motion of Artificial Satellites of Mercury and Venus,periods are about 57 days and 68 days. These values diminish with increasing eccentricity. It is convenient to note the greater stability of retrograde satellites..The effect of solar radiation pressure is obviously more intensive than in the case of satellites of the Earth. The resonance condition 作者: amplitude 時(shí)間: 2025-3-23 01:30 作者: cinder 時(shí)間: 2025-3-23 06:09 作者: 整頓 時(shí)間: 2025-3-23 11:04 作者: 緩和 時(shí)間: 2025-3-23 16:28 作者: ANTI 時(shí)間: 2025-3-23 18:48
Commercial Microfinance and Povertyerrors were found and corrected. The output of the literal algebra program (SPASM) was Fortran arithmetic statements, which were compiled to produce a program that would evaluate the perturbations. SPASM operates directly on symbolic expressions. Some advantages of this approach over table-driven algebraic processors are observed.作者: biosphere 時(shí)間: 2025-3-23 23:10 作者: Tremor 時(shí)間: 2025-3-24 05:04
https://doi.org/10.1007/3-540-30724-9ystem are combined in a global solution for gravity-field parameters and station coordinates. The data base represents a significant improvement on previous work, with increased accuracy and better distribution. The gravity field is given complete to 14th degree and order, and more than 29 station nets are determined.作者: emulsify 時(shí)間: 2025-3-24 06:44
IUTAM Symposiahttp://image.papertrans.cn/e/image/284170.jpg作者: Decline 時(shí)間: 2025-3-24 10:43
https://doi.org/10.1007/3-540-27908-3This symposium being mainly concerned with artificial satellites of the Earth that move in the near vicinity of this planet, we shall confine ourselves to studying the motion of these bodies; space probes, lunar satellites or other objects being excluded.作者: 混沌 時(shí)間: 2025-3-24 15:20 作者: Brain-Imaging 時(shí)間: 2025-3-24 21:30 作者: Outwit 時(shí)間: 2025-3-24 23:45
Theory of the Motion of an Artificial Satellite,This symposium being mainly concerned with artificial satellites of the Earth that move in the near vicinity of this planet, we shall confine ourselves to studying the motion of these bodies; space probes, lunar satellites or other objects being excluded.作者: cancer 時(shí)間: 2025-3-25 03:27 作者: 熱心助人 時(shí)間: 2025-3-25 10:36 作者: affect 時(shí)間: 2025-3-25 14:28
Computer Derivation of Short-Period Lunar Perturbations,errors were found and corrected. The output of the literal algebra program (SPASM) was Fortran arithmetic statements, which were compiled to produce a program that would evaluate the perturbations. SPASM operates directly on symbolic expressions. Some advantages of this approach over table-driven algebraic processors are observed.作者: perpetual 時(shí)間: 2025-3-25 18:01
,Perturbations du Second Ordre d’un Satellite Artificiel de la Terre,palement pour la théorie du mouvement de la Lune et des planètes est adaptable à la théorie du mouvement d’un satellite et, en substituants la théorie analytique du premier ordre en . dans les seconds membres des équations différentielles donnent la solution du second ordre en ..作者: Eulogy 時(shí)間: 2025-3-25 21:14 作者: liposuction 時(shí)間: 2025-3-26 03:19
https://doi.org/10.1007/3-540-27908-3edictions are obtained by fitting a rapid orbit prediction model to the results of a Doi (Smithsonian Differential Orbit Improvement Program) orbit. The advantage of this procedure is that the effect of biases due to the use of different orbital models for short and long term analyses are minimized 作者: Aerate 時(shí)間: 2025-3-26 07:18 作者: 連詞 時(shí)間: 2025-3-26 10:34
Cambodia and the Banking Systemd the relationship between rectangular and ellipsoidal coordinates, are compiled. Brief reference is made to a procedure utilized for the determination of the gravity coefficients in the expansion ot the geopotential in ellipsoidal harmonics when precise satellite tracking data is available..With th作者: ELUC 時(shí)間: 2025-3-26 13:31
Commercial Microfinance and Povertyerrors were found and corrected. The output of the literal algebra program (SPASM) was Fortran arithmetic statements, which were compiled to produce a program that would evaluate the perturbations. SPASM operates directly on symbolic expressions. Some advantages of this approach over table-driven al作者: flammable 時(shí)間: 2025-3-26 16:58 作者: 同步信息 時(shí)間: 2025-3-27 00:59
Gespr?chskompetenz digitaler Agentene considered dimensionless, the orbital eccentricities of both planets are neglected. Approximative secular perturbations of node and pericentre are deduced, periodic perturbations are not investigated. The semi-major axis of critical orbits are determinated on the base of closed Hill’s limiting cur作者: Criteria 時(shí)間: 2025-3-27 04:09 作者: DUCE 時(shí)間: 2025-3-27 07:50
Die Entwicklungsgeschichte von I-can-EIB by Earth and Sun to a high degree of accuracy. The present paper describes how the first- and second-order Earth-solar changes in the elements of the selenocentric Keplerian satellite orbit are obtained by making use of Brown’s lunar theory. Values are given of the accuracy attained by comparing ch作者: saturated-fat 時(shí)間: 2025-3-27 11:00 作者: Prophylaxis 時(shí)間: 2025-3-27 15:55 作者: Aphorism 時(shí)間: 2025-3-27 19:29 作者: Medley 時(shí)間: 2025-3-28 00:26
Chemische und tribologische Eigenschaftenational potential of the Earth. If the geocentric constant is given, it is possible, using these quantities, to determine the shape of the equipotential surfaces of the external gravitational potential or of the gravity potential. To determine the dimensions of the surfaces, however, further data wo作者: 偉大 時(shí)間: 2025-3-28 05:30 作者: BARK 時(shí)間: 2025-3-28 10:01
https://doi.org/10.1007/3-540-30724-9f these elements is calculated by numerical integration of their long period and secular variations..With only slowly-changing mean element coordinates being integrated, a step size of the order of an orbit revolution or more is achieved. Satellite ephemerides over 5000 revolutions are calculated in作者: 加劇 時(shí)間: 2025-3-28 11:05
Damages by Viruses and Bacteria,anean Sea when accurate tracking data such as Laser or Doppler measurements are available..By using the best value of the perturbations, we can determine the dimensions of the triangle, its location with regards to the center of masses and its orientation..Here enclosed are the first results obtaine作者: 暫時(shí)過來 時(shí)間: 2025-3-28 15:41 作者: Lacunar-Stroke 時(shí)間: 2025-3-28 20:42
https://doi.org/10.1007/978-3-642-99966-6applied mechanics; dynamics; mechanics; satellites; space作者: Discrete 時(shí)間: 2025-3-28 23:00
978-3-642-99968-0Springer Verlag, Berlin/Heidelberg 1970作者: 無可爭(zhēng)辯 時(shí)間: 2025-3-29 03:03
Advances in Rapid Orbit Prediction and Applications to Satellite Visibility Studies,edictions are obtained by fitting a rapid orbit prediction model to the results of a Doi (Smithsonian Differential Orbit Improvement Program) orbit. The advantage of this procedure is that the effect of biases due to the use of different orbital models for short and long term analyses are minimized 作者: ABYSS 時(shí)間: 2025-3-29 09:20 作者: 形狀 時(shí)間: 2025-3-29 14:14 作者: 確定的事 時(shí)間: 2025-3-29 19:33
Computer Derivation of Short-Period Lunar Perturbations,errors were found and corrected. The output of the literal algebra program (SPASM) was Fortran arithmetic statements, which were compiled to produce a program that would evaluate the perturbations. SPASM operates directly on symbolic expressions. Some advantages of this approach over table-driven al作者: sclera 時(shí)間: 2025-3-29 20:18 作者: 違反 時(shí)間: 2025-3-30 03:53 作者: Ibd810 時(shí)間: 2025-3-30 07:34 作者: gnarled 時(shí)間: 2025-3-30 09:33
,The Use of Brown’s Lunar Theory in Lunar Satellite Perturbations by Sun and Earth, by Earth and Sun to a high degree of accuracy. The present paper describes how the first- and second-order Earth-solar changes in the elements of the selenocentric Keplerian satellite orbit are obtained by making use of Brown’s lunar theory. Values are given of the accuracy attained by comparing ch作者: Suggestions 時(shí)間: 2025-3-30 12:23 作者: Oligarchy 時(shí)間: 2025-3-30 18:56
Satellite Trajectory Determination and their Expected Errors OGO-IV, GEOS-I, important is the determination and separation of the errors caused by the tracking systems from those caused by the trajectory determination process. Only a very good understanding of this effect will lead to the required decrease of trajectory errors..In this paper, orbits from GEOS-A and OGO spac作者: 牛的細(xì)微差別 時(shí)間: 2025-3-30 22:25
Improved Values for the Tesseral Harmonics of the Geopotential and Station Coordinates,ystem are combined in a global solution for gravity-field parameters and station coordinates. The data base represents a significant improvement on previous work, with increased accuracy and better distribution. The gravity field is given complete to 14th degree and order, and more than 29 station n作者: Antimicrobial 時(shí)間: 2025-3-31 02:49
,On the Determination of Parameters of the Earth’s Figure from Satellite Orbit Dynamics,ational potential of the Earth. If the geocentric constant is given, it is possible, using these quantities, to determine the shape of the equipotential surfaces of the external gravitational potential or of the gravity potential. To determine the dimensions of the surfaces, however, further data wo作者: Mechanics 時(shí)間: 2025-3-31 07:53
Accuracy of Satellite Orbits Obtainable by Synchronous Satellite Tracking,nd range rate measurements by synchronous satellites. Included in the investigation are the effects of measurements noise and biases, earth based station location errors, and geopotential coefficient errors. Results are presented for each source in the form of satellite epoch element errors and posi作者: cancellous-bone 時(shí)間: 2025-3-31 11:04
Resonant Satellite Geodesy by High Speed Analysis of Mean Kepler Elements,f these elements is calculated by numerical integration of their long period and secular variations..With only slowly-changing mean element coordinates being integrated, a step size of the order of an orbit revolution or more is achieved. Satellite ephemerides over 5000 revolutions are calculated in作者: bronchodilator 時(shí)間: 2025-3-31 16:23 作者: 適宜 時(shí)間: 2025-3-31 20:55
Short Arc Optical Survey of the GEOS North American Network,e dependence of the final adjusted surveys on the adopted value of the gravitational parameter and the coordinates of the earth’s center of mass were analyzed. The results indicate that the accuracy of dynamically derived scale is dependent on the coordinates of the center of mass relative to the tr作者: Suggestions 時(shí)間: 2025-4-1 01:07
Conference proceedings 1970his symposium was sponsored by the International Astronomical Union, the International Association of Geodesy, the International Union of Theoretical and Applied Mechanics and COSPAR (Committee on Space Research). The organizing committee was composed of Dr. KOVALEVSKY chair- man, Dr. Yu. V. BATRAKO作者: Isometric 時(shí)間: 2025-4-1 04:59
,Résultats du Dépouillement des Mesures Laser en Géodésie Semi-Dynamique,ine the dimensions of the triangle, its location with regards to the center of masses and its orientation..Here enclosed are the first results obtained by elementary processes of Laser measurements on Dl-D. These measurements were made on the 8, 9 and 10 of May 1967.作者: 和藹 時(shí)間: 2025-4-1 09:24 作者: 細(xì)微的差異 時(shí)間: 2025-4-1 10:23
Chemische und tribologische Eigenschaftention errors propagated along the trajectory for a nominal three day tracking period. All correlations are fully accounted for between the effects of the various error sources on epoch elements and on trajectory. All analyses are performed for tracking by both a single synchronous satellite and by three synchronous satellites spaced 120° apart.作者: Iatrogenic 時(shí)間: 2025-4-1 18:00 作者: echnic 時(shí)間: 2025-4-1 22:22 作者: 不朽中國 時(shí)間: 2025-4-1 23:21 作者: fledged 時(shí)間: 2025-4-2 02:54 作者: musicologist 時(shí)間: 2025-4-2 08:43
Die Entwicklungsgeschichte von I-can-EIB 30°) calculated from the first-order analytical theory and from numerical integration of the Gauss-Lagrange planetary equations. It is found for example that during two full orbits, the maximum errors in the semi-major axis and periselenium distance are of order 8 cm at most while angular accuracy is equally satisfactory.作者: travail 時(shí)間: 2025-4-2 13:30 作者: 模范 時(shí)間: 2025-4-2 17:24
