標(biāo)題: Titlebook: Dynamics of Natural and Artificial Celestial Bodies; Proceedings of the U Halina Pretka-Ziomek,Edwin Wnuk,David L. Richardso Conference pro [打印本頁] 作者: protocol 時(shí)間: 2025-3-21 16:38
書目名稱Dynamics of Natural and Artificial Celestial Bodies影響因子(影響力)
書目名稱Dynamics of Natural and Artificial Celestial Bodies影響因子(影響力)學(xué)科排名
書目名稱Dynamics of Natural and Artificial Celestial Bodies網(wǎng)絡(luò)公開度
書目名稱Dynamics of Natural and Artificial Celestial Bodies網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Dynamics of Natural and Artificial Celestial Bodies被引頻次
書目名稱Dynamics of Natural and Artificial Celestial Bodies被引頻次學(xué)科排名
書目名稱Dynamics of Natural and Artificial Celestial Bodies年度引用
書目名稱Dynamics of Natural and Artificial Celestial Bodies年度引用學(xué)科排名
書目名稱Dynamics of Natural and Artificial Celestial Bodies讀者反饋
書目名稱Dynamics of Natural and Artificial Celestial Bodies讀者反饋學(xué)科排名
作者: archaeology 時(shí)間: 2025-3-21 21:24 作者: 我不死扛 時(shí)間: 2025-3-22 02:27 作者: commensurate 時(shí)間: 2025-3-22 07:03
Changes in Rotational Angular Momentum Due to Gravitational Interactions Between Two Finite Bodies of the change in rotational angular momentum of the non-spherical body are derived over one interaction (i.e. periapsis passage) between the bodies. The estimated changes are expressed in terms of trigonometric functions and generalized Hansen coefficients.作者: TOM 時(shí)間: 2025-3-22 11:17 作者: Adenoma 時(shí)間: 2025-3-22 15:46
Formation Flying Satellites: Control by an Astrodynamicistng Hill’s (or Clohessy Wiltshire) equations. Unfortunately the gravitational perturbations destroy the periodicity of the orbits and control will be required to maintain the desired orbits. Since fuel will be one of the major factors limiting the system lifetime it is imperative that fuel consumptio作者: Adenoma 時(shí)間: 2025-3-22 18:28
Low Energy Transfer to the Moonnsfer. In this paper, we apply the dynamical systems techniques developed in our earlier work to reproduce systematically a Hiten-like mission. We approximate the Sun—Earth—Moon-spacecraft 4-body system as two 3-body systems. Using the invariant manifold structures of the Lagrange points of the 3-bo作者: colostrum 時(shí)間: 2025-3-23 00:12
Dissipative Forces and External Resonancesase of external mean motion resonances. The numerical simulations presented are computed by using the 3-dimensional extended Schubart averaging (ESA) integrator developed by Moons (1994) for all mean motion resonances. We complete it by adding the contributions of the dissipative forces. To follow t作者: 虛弱的神經(jīng) 時(shí)間: 2025-3-23 05:17 作者: CLOWN 時(shí)間: 2025-3-23 05:40 作者: 樣式 時(shí)間: 2025-3-23 10:22 作者: craving 時(shí)間: 2025-3-23 16:55
New Estimation of Usually Neglected Forces Acting on Galilean Systeme the ephemeris of these satellites which are outside the precision of the observations. We used a numerical method to test the effect of such perturbations. Here are reporting the main results we obtained.作者: blackout 時(shí)間: 2025-3-23 20:53 作者: Ballad 時(shí)間: 2025-3-24 00:50
On the Relationship Between Fast Lyapunov Indicator and Periodic Orbits for Symplectic Mappingsws to discriminate between ordered and weak chaotic motion and also, under certain conditions, between resonant and non resonant regular orbits. The aim of this paper is to study numerically the relationship between the Fast Lyapunov Indicator values and the order of periodic orbits. Using the two-d作者: Affiliation 時(shí)間: 2025-3-24 04:39
On the Observability of Radiation Forces Acting on Near-Earth Asteroids radar astrometric observations at multiple apparitions, spanning periods on the order of 10 years, allows the detection of such forces on bodies as large as kilometer across. Indeed, the perturbations are so substantial that certain of the forces can be essential to fit an orbit to the observations作者: RAGE 時(shí)間: 2025-3-24 08:37 作者: 昏暗 時(shí)間: 2025-3-24 10:57
Attitude Dynamics of Orbiting Gyrostatsoncanonical Hamiltonian system, where the Hamiltonian includes the potential, a volume integral over the body of the gyrostat. In practice, the Hamiltonian is approximated to partially decouple the position and attitude equations. The equilibria of this system of equations represent the steady motio作者: 后來 時(shí)間: 2025-3-24 18:24
Conference proceedings 2001niversity in Poznan, Poland and held in Poznan, from 3 to 7 July 2000. The purpose of the workshop was to identify future research in celestial mech- anics and encourage collaboration among scientists from eastem and westem coun- tries. There was a full program of invited and contributed presentatio作者: Confidential 時(shí)間: 2025-3-24 21:05 作者: anniversary 時(shí)間: 2025-3-24 23:56 作者: RENAL 時(shí)間: 2025-3-25 04:40
Formation Flying Satellites: Control by an Astrodynamicistel consumption and this average amount needs to be minimized. Thus, control of the system has to be addressed, not just control of each satellite. In this paper control of the individual satellites as well as the constellation is addressed from an astrodynamics perspective.作者: Jargon 時(shí)間: 2025-3-25 11:30
Attitude Dynamics of Orbiting Gyrostats algorithm for computing equilibria. In contrast to other approaches, this algorithm provides stability information directly, since the calculations required to solve the constrained minimization problem are also involved in computing the positive definiteness of the Hamiltonian as a Lyapunov function.作者: 倔強(qiáng)不能 時(shí)間: 2025-3-25 14:32 作者: 類人猿 時(shí)間: 2025-3-25 18:41
Low Energy Transfer to the Moondy systems, we are able to construct low energy transfer trajectories from the Earth which execute ballistic capture at the Moon. The techniques used in the design and construction of this trajectory may be applied in many situations.作者: Inflamed 時(shí)間: 2025-3-25 20:43 作者: 表臉 時(shí)間: 2025-3-26 03:30
Lunisolar Resonances Revisitedg an appropriate fundamental model to each case. Only a part of resonances match known fundamental models. An extended fundamental model is proposed to account for some complicated phenomena. Most of the double resonance cases still remain unexplored.作者: aviator 時(shí)間: 2025-3-26 04:21 作者: 生意行為 時(shí)間: 2025-3-26 11:01 作者: 逃避責(zé)任 時(shí)間: 2025-3-26 14:11
Teresa Gómez Reus,Terry Gifford only few terms a good approximation is obtained. Once the expansion is performed, it is possible to apply to it a Lie-transformation. An application to a tri-axial rigid body moving in a Keplerian orbit is made.作者: 合并 時(shí)間: 2025-3-26 20:01
Origins of the Congress of Westphaliady systems, we are able to construct low energy transfer trajectories from the Earth which execute ballistic capture at the Moon. The techniques used in the design and construction of this trajectory may be applied in many situations.作者: 最高點(diǎn) 時(shí)間: 2025-3-26 23:07
Origins of the Congress of Westphaliahe philosophy of the initial integrator, we average the drag terms, but we do not make any expansion in series of eccentricity or inclination. We show our results, especially capture around asymmetric equilibria, and compare them to those found by Beaué and Ferraz-Mello (1993, 1994) and Liou et al. (1979).作者: 補(bǔ)角 時(shí)間: 2025-3-27 02:55
Origins of the Congress of Westphaliag an appropriate fundamental model to each case. Only a part of resonances match known fundamental models. An extended fundamental model is proposed to account for some complicated phenomena. Most of the double resonance cases still remain unexplored.作者: Offset 時(shí)間: 2025-3-27 06:16 作者: 我沒有強(qiáng)迫 時(shí)間: 2025-3-27 12:01
Introduction: The Evolved Workplace,plain the relationship that we have found between the values of the Fast Lyapunov Indicator, the order of the periodic orbits and also the minimum number of iterations needed to obtain the Fast Lyapunov Indicator values.作者: Jacket 時(shí)間: 2025-3-27 14:06
On the Relationship Between Fast Lyapunov Indicator and Periodic Orbits for Symplectic Mappingsplain the relationship that we have found between the values of the Fast Lyapunov Indicator, the order of the periodic orbits and also the minimum number of iterations needed to obtain the Fast Lyapunov Indicator values.作者: 乳汁 時(shí)間: 2025-3-27 18:55
ckiewicz University in Poznan, Poland and held in Poznan, from 3 to 7 July 2000. The purpose of the workshop was to identify future research in celestial mech- anics and encourage collaboration among scientists from eastem and westem coun- tries. There was a full program of invited and contributed p作者: 披肩 時(shí)間: 2025-3-27 23:55
Introduction: The Evolved Workplace, orbits present in some models is of particular interest because it rises, on the one hand, the question of the origin of those chaotic motions and, on the other hand, the question of whether an equilibrium stellar system can be built when the bulk of the stars that make it up behave chaotically.作者: GAVEL 時(shí)間: 2025-3-28 03:29 作者: 旋轉(zhuǎn)一周 時(shí)間: 2025-3-28 08:37
Origins of the Congress of Westphaliaing that the stiffness of the ring is large and the dissipation is small enough, we study the quasi-static motion which is set in after free elastic oscillations have damped. In particular, the steady-state motions in the weakly elliptic orbit are found and their stability is investigated.作者: Dna262 時(shí)間: 2025-3-28 13:02 作者: WAIL 時(shí)間: 2025-3-28 15:34
Introduction: The Evolved Workplace,e show that the generic occurrence of rings for the case of rotating short-range potentials can be extended to the case of gravitational potentials. The consecutive collision periodic orbits created by saddle-center bifurcations are of central importance.作者: Coma704 時(shí)間: 2025-3-28 20:13
Origins of the Congress of WestphaliaThe problem of three bodies when one of them is a gyrostat is considered. Using the symmetries of the system we carry out two reductions. Global considerations about the conditions for relative equilibria are made. Finally, we restrict to an approximated model of the dynamics and a complete study of the relative equilibria is made.作者: idiopathic 時(shí)間: 2025-3-28 23:58
Introduction: The Evolved Workplace,Rotational motion of a rigid satellite moving in a circular orbit around an oblate planet is considered. For a case of a symmetric satellite, we prove non-integrability of equations of motion applying Morales-Ramis extension of Ziglin theory.作者: 混合,攙雜 時(shí)間: 2025-3-29 04:03 作者: Range-Of-Motion 時(shí)間: 2025-3-29 11:11
Non-Integrability of a Certain Problem of Rotational Motion of a Rigid SatelliteRotational motion of a rigid satellite moving in a circular orbit around an oblate planet is considered. For a case of a symmetric satellite, we prove non-integrability of equations of motion applying Morales-Ramis extension of Ziglin theory.作者: foppish 時(shí)間: 2025-3-29 15:00 作者: conception 時(shí)間: 2025-3-29 17:16 作者: investigate 時(shí)間: 2025-3-29 23:08
Teresa Gómez Reus,Terry Gifford inside the orbit of Jupiter and vice versa. During this transition, the comet can be captured temporarily by Jupiter for one to several orbits around Jupiter. The interior heliocentric orbit is typically close to the 3:2 resonance while the exterior heliocentric orbit is near the 2:3 resonance. An 作者: 針葉 時(shí)間: 2025-3-30 00:05 作者: Feedback 時(shí)間: 2025-3-30 06:36 作者: infantile 時(shí)間: 2025-3-30 08:48
Origins of the Congress of Westphaliang Hill’s (or Clohessy Wiltshire) equations. Unfortunately the gravitational perturbations destroy the periodicity of the orbits and control will be required to maintain the desired orbits. Since fuel will be one of the major factors limiting the system lifetime it is imperative that fuel consumptio作者: apropos 時(shí)間: 2025-3-30 16:02 作者: Licentious 時(shí)間: 2025-3-30 16:48 作者: GLADE 時(shí)間: 2025-3-30 21:15 作者: 上坡 時(shí)間: 2025-3-31 03:54
Introduction: The Evolved Workplace,or small numbers of observations. The techniques rely on the orbital element probability density computed using statistical orbital ranging. We apply the techniques to the Earth-crossing asteroid 1998 OX. with non-vanishing collision probability in numerous close approaches after the year 2012 (incl作者: 改變 時(shí)間: 2025-3-31 07:28 作者: 陰謀 時(shí)間: 2025-3-31 10:26 作者: 平庸的人或物 時(shí)間: 2025-3-31 13:20
Introduction: The Evolved Workplace,e show that the generic occurrence of rings for the case of rotating short-range potentials can be extended to the case of gravitational potentials. The consecutive collision periodic orbits created by saddle-center bifurcations are of central importance.作者: Suggestions 時(shí)間: 2025-3-31 20:00 作者: Interdict 時(shí)間: 2025-4-1 01:06
Introduction: The Evolved Workplace, radar astrometric observations at multiple apparitions, spanning periods on the order of 10 years, allows the detection of such forces on bodies as large as kilometer across. Indeed, the perturbations are so substantial that certain of the forces can be essential to fit an orbit to the observations作者: follicle 時(shí)間: 2025-4-1 02:57 作者: 灰姑娘 時(shí)間: 2025-4-1 09:51 作者: deactivate 時(shí)間: 2025-4-1 12:22
Changes in Rotational Angular Momentum Due to Gravitational Interactions Between Two Finite Bodies of the change in rotational angular momentum of the non-spherical body are derived over one interaction (i.e. periapsis passage) between the bodies. The estimated changes are expressed in terms of trigonometric functions and generalized Hansen coefficients.作者: 鳥籠 時(shí)間: 2025-4-1 15:55
Quasi-Static Motions of Viscoelastic Satellitesing that the stiffness of the ring is large and the dissipation is small enough, we study the quasi-static motion which is set in after free elastic oscillations have damped. In particular, the steady-state motions in the weakly elliptic orbit are found and their stability is investigated.
