突然
发表于 2025-3-21 19:37:32
书目名称Orbital Relative Motion and Terminal Rendezvous影响因子(影响力)<br> http://impactfactor.cn/if/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous影响因子(影响力)学科排名<br> http://impactfactor.cn/ifr/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous网络公开度<br> http://impactfactor.cn/at/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous网络公开度学科排名<br> http://impactfactor.cn/atr/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous被引频次<br> http://impactfactor.cn/tc/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous被引频次学科排名<br> http://impactfactor.cn/tcr/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous年度引用<br> http://impactfactor.cn/ii/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous年度引用学科排名<br> http://impactfactor.cn/iir/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous读者反馈<br> http://impactfactor.cn/5y/?ISSN=BK0703594<br><br> <br><br>书目名称Orbital Relative Motion and Terminal Rendezvous读者反馈学科排名<br> http://impactfactor.cn/5yr/?ISSN=BK0703594<br><br> <br><br>
optional
发表于 2025-3-21 22:46:05
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
Misgiving
发表于 2025-3-22 01:58:21
http://reply.papertrans.cn/71/7036/703594/703594_3.png
LAVA
发表于 2025-3-22 04:57:09
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
无礼回复
发表于 2025-3-22 09:51:36
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. .
HAVOC
发表于 2025-3-22 15:43:11
http://reply.papertrans.cn/71/7036/703594/703594_6.png
混合物
发表于 2025-3-22 19:48:12
Space Technology Libraryhttp://image.papertrans.cn/o/image/703594.jpg
foppish
发表于 2025-3-22 23:28:14
http://reply.papertrans.cn/71/7036/703594/703594_8.png
我说不重要
发表于 2025-3-23 04:42:06
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 to obtain analytic expression for the spacecraft motion perturbed by the luni-solar gravity.
灯泡
发表于 2025-3-23 09:33:02
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 by Kwok.