標(biāo)題: Titlebook: Orbital Relative Motion and Terminal Rendezvous; Analytic and Numeric Jean Albert Kéchichian Book 2021 The Editor(s) (if applicable) and Th [打印本頁(yè)] 作者: 突然 時(shí)間: 2025-3-21 19:37
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書目名稱Orbital Relative Motion and Terminal Rendezvous影響因子(影響力)學(xué)科排名
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書目名稱Orbital Relative Motion and Terminal Rendezvous網(wǎng)絡(luò)公開(kāi)度學(xué)科排名
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書目名稱Orbital Relative Motion and Terminal Rendezvous讀者反饋學(xué)科排名
作者: optional 時(shí)間: 2025-3-21 22:46
The Second-Order Analytic Approximation to the Solution of the Euler-Hill Equations of Relative Motfrom the origin of the frame, it is felt that because of the presence of initial non-zero velocities, the subsequent motion may drift to considerable distances from the origin of the frame, thereby, degrading the accuracy of the analytic first-order solution of the equations of motion. The initial v作者: Misgiving 時(shí)間: 2025-3-22 01:58 作者: LAVA 時(shí)間: 2025-3-22 04:57
The Analysis and Implementation of In-Plane Stationkeeping of Continuously Perturbed Walker Constelgiven tolerance deadband is about to be violated. This chapter illustrates the computations associated with the stationkeeping of a generic Walker constellation, by maneuvering each leading spacecraft within an orbit plane, and calculating the associated velocity changes required for controlling the作者: 無(wú)禮回復(fù) 時(shí)間: 2025-3-22 09:51
Book 2021liptic orbit case..The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics,and students at the graduate level and above.?.作者: HAVOC 時(shí)間: 2025-3-22 15:43 作者: 混合物 時(shí)間: 2025-3-22 19:48
Space Technology Libraryhttp://image.papertrans.cn/o/image/703594.jpg作者: foppish 時(shí)間: 2025-3-22 23:28 作者: 我說(shuō)不重要 時(shí)間: 2025-3-23 04:42
Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influturbed by Earth’s . and . zonals, and described in the rotating Euler-Hill frame, the same approach is used in this chapter and based on Reference [2] to obtain analytic expression for the spacecraft motion perturbed by the luni-solar gravity.作者: 燈泡 時(shí)間: 2025-3-23 09:33
The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis PrograThis chapter shows the equations used in the JPL computer program ASAP that are specific to the modeling of the central body disturbing function, the third-body disturbing function, as well as the equations of motion due to atmospheric drag. These descriptions are taken directly from Reference [1] by Kwok.作者: BOOST 時(shí)間: 2025-3-23 12:24 作者: extemporaneous 時(shí)間: 2025-3-23 14:02
Orbital Relative Motion and Terminal Rendezvous978-3-030-64657-8Series ISSN 0924-4263 Series E-ISSN 2542-8896 作者: OCTO 時(shí)間: 2025-3-23 18:21
Book 2021ives. The first is to derive the mathematics of relative motion in near-circular orbit when subjected to perturbations emanating from the oblateness of the Earth, third-body gravity, and atmospheric drag. The mathematics are suitable for quick trajectory prediction and the creation of computer codes作者: 喃喃訴苦 時(shí)間: 2025-3-23 22:18 作者: critique 時(shí)間: 2025-3-24 02:21 作者: cogent 時(shí)間: 2025-3-24 08:57
Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influthe . harmonic, a position error of 200?m per revolution is sustained when the initial orbit is circular. The equations developed in this chapter can be used to carry out terminal rendezvous in near-circular obit around the oblate Earth.作者: cloture 時(shí)間: 2025-3-24 14:12
The Analysis of the Relative Motion in General Elliptic Orbit with Respect to a Dragging and Precese equations can be effectively put to use in calculating by an iterative scheme, the impulsive rendezvous maneuvers in elliptic orbit around the Earth or those planets that are either atmosphere bearing or have a dominant second zonal harmonic, or both.作者: 愛(ài)了嗎 時(shí)間: 2025-3-24 16:39 作者: 阻撓 時(shí)間: 2025-3-24 21:48
Effect of Luni-Solar Gravity Perturbations on a Near-Circular Orbit: Third-Body Orbit Eccentricity ied out, all the orbital elements can be readily obtained and used for example in the maneuver planning function. This theory can be useful for the autonomous navigation of geostationary spacecraft as well as other high near-circular orbit applications such as the GPS spacecraft.作者: consolidate 時(shí)間: 2025-3-25 03:03 作者: 沙發(fā) 時(shí)間: 2025-3-25 06:25 作者: Guileless 時(shí)間: 2025-3-25 08:23
The Second-Order Analytic Approximation to the Solution of the Euler-Hill Equations of Relative Mote numerically integrated exact solution, at greater distances from the origin of the rotating reference frame. These solutions have been developed to study the problem of the terminal rendezvous guidance where an active spacecraft at several hundred km from its rendezvous target centered at the rota作者: 替代品 時(shí)間: 2025-3-25 13:13
Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influ small eccentricity and arbitrary inclination, energy, node and perigee location is analyzed. The second-order Euler-Hill differential equations are solved after expanding the forcing terms to first-order in the small parameter defining the orbit eccentricity. The construction of the circular refere作者: Ovulation 時(shí)間: 2025-3-25 17:27
Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influturbed by Earth’s . and . zonals, and described in the rotating Euler-Hill frame, the same approach is used in this chapter and based on Reference [2] to obtain analytic expression for the spacecraft motion perturbed by the luni-solar gravity.作者: Eviction 時(shí)間: 2025-3-25 21:05
Effect of Luni-Solar Gravity Perturbations on a Near-Circular Orbit: Third-Body Orbit Eccentricity rder to simplify the analysis, the lunar as well as the apparent solar orbits were assumed to be circular. In this chapter, this assumption is removed such that the third-body orbits are now allowed to describe Keplerian ellipses. Second and higher-order terms in the eccentricities of the lunar and 作者: Gum-Disease 時(shí)間: 2025-3-26 01:04
Effect of Atmospheric Drag Perturbation on Circular Orbits: Atmosphere Rotation Considerations,nergy, and perigee location and small eccentricity. Following the practice used in References [1, 2], and the preceding chapters, the rotating Euler-Hill frame is used to describe the perturbed motion of the spacecraft by assuming that the atmospheric density obeys an exponential decay law with radi作者: 消瘦 時(shí)間: 2025-3-26 07:38 作者: 得意人 時(shí)間: 2025-3-26 11:51
Techniques of Accurate Analytic Terminal Rendezvous in Near-Circular Orbit,ed to the active maneuvering vehicle is determined with high accuracy, such that, the error in interceptmg the passive spacecraft in a given time is negligible. This error is evaluated by numerically integrating both spacecraft orbits, by accounting for the second zonal harmonic .. A typical large t作者: mortgage 時(shí)間: 2025-3-26 14:59
Coplanar Two-Impulse Rendezvous in General Elliptic Orbit with Drag,ral elliptic orbit is presented in this chapter. The motion of the passive vehicle is described by the inverse square gravitational field of the primary body and by atmospheric drag. The center of a rotating reference frame is attached to this vehicle, and the motion of the active maneuvering vehicl作者: 統(tǒng)治人類 時(shí)間: 2025-3-26 17:51
The Analysis of the Relative Motion in General Elliptic Orbit with Respect to a Dragging and Preces in general elliptic orbit, relative to a rotating reference frame which drags and precesses exactly as a given spacecraft attached to its center is derived. This attached spacecraft is itself flying a general elliptic orbit and can be considered as the passive or non-maneuvering vehicle. The unaver作者: 松軟 時(shí)間: 2025-3-26 22:30
The Algorithm of the Two-Impulse Time-Fixed Noncoplanar Rendezvous with Drag and Oblateness Effectsmotion of the maneuvering spacecraft is referred to a rotating reference frame attached to the passive spacecraft, and dragging and precessing at the same rate as that spacecraft. An iterative scheme is devised to find the magnitude and orientation of the initiating impulse that brings the active sp作者: 退出可食用 時(shí)間: 2025-3-27 01:16 作者: NAIVE 時(shí)間: 2025-3-27 06:18 作者: 灌溉 時(shí)間: 2025-3-27 12:12 作者: 休閑 時(shí)間: 2025-3-27 15:13 作者: 我不死扛 時(shí)間: 2025-3-27 18:25
Eva Hoffmann he was able to undergo matrimony, and consequently the Kingdom of Heaven was left unopened. Because the Lord of the Second Advent is believed to have taken over the unfulfilled mission of Jesus, Sun Myung Moon is accorded the achievement of inaugurating a new era of human history — the Completed Te作者: RLS898 時(shí)間: 2025-3-28 01:13
The Impact of Fintech Phenomenon on Economic Development: The Case of Bahrainof Bahrain FinTech Bay and Central Bank of Bahrain in terms of regulations, operations and monitoring the establishment cycle of electronic payment systems. This study examines the impact of the newly electronic payment systems on Bahrain economy development due to the high demand for digital paymen作者: 破譯 時(shí)間: 2025-3-28 02:57
Preparing Libraries in ,d subcloning (.). PCR products are digested with restriction endonucleases, ligated into an expression vector digested with the same enzymes, and the resultant recombinant plasmids are transformed into supercompetent bacteria. One difference between routine subcloning of a single gene and preparing 作者: 保全 時(shí)間: 2025-3-28 08:39 作者: connoisseur 時(shí)間: 2025-3-28 14:00
Therapies Used in Psychosexual Care,a 10-session group behavioural therapy or a control group. Men who participated in the group therapy reported improved sexual functioning compared with controls [1]. This highlights something that the pathway could focus on and has been shown to have a positive impact.作者: Perceive 時(shí)間: 2025-3-28 16:20
AppFabric: Caching,re, the fact that load balancing can only be done in a round-robin fashion certainly has architectural impact, especially when pitted against the fact that two instances must be running to remain within the terms of the Azure Service Level Agreement. This is where customers typically realize what I 作者: 歌劇等 時(shí)間: 2025-3-28 18:52 作者: 一再遛 時(shí)間: 2025-3-28 23:39
Using Smart Cards in an Educational Environment application for an Educational Institute, together with the resulting benefits for both the students and the institute. A detailed description of the way that the smart card security features have been capitalised for implementing certification and authentication mechanisms is also provided.作者: 煩人 時(shí)間: 2025-3-29 06:58 作者: FRET 時(shí)間: 2025-3-29 08:16 作者: brother 時(shí)間: 2025-3-29 11:28 作者: 誘使 時(shí)間: 2025-3-29 19:08 作者: PACK 時(shí)間: 2025-3-29 20:46
Hauptuntersuchungive and problem-solving skills . .Lays a foundation for success and fun with LEGO MINDSTORMS NXT 2.0...Please note: .the print version of this title is black & white; the eBook is full color..978-1-4302-2491-4978-1-4302-2492-1作者: Prosaic 時(shí)間: 2025-3-30 01:18
Book‘‘‘‘‘‘‘‘ 2015urement of radiation emission from an otolith section to identify the main period of contaminationin fish. The FNPP accident represents a rare instance where the environmental radioactivity level was elevated steeply through atmospheric fallout and direct discharge of radioactive water into the sea 作者: Bucket 時(shí)間: 2025-3-30 05:57 作者: 異常 時(shí)間: 2025-3-30 11:59
