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Titlebook: Astrodynamics Network AstroNet-II; The Final Conference Gerard Gómez,Josep J. Masdemont Conference proceedings 2016 Springer International

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樓主: Spouse
51#
發(fā)表于 2025-3-30 08:15:16 | 只看該作者
52#
發(fā)表于 2025-3-30 14:38:26 | 只看該作者
53#
發(fā)表于 2025-3-30 17:21:21 | 只看該作者
Brian Fitzgerald,Debra HowcroftSolar Radiation Pressure (SRP). The system has a family of “artificial” equilibrium points parameterised by the orientation of the sail. We show how to use the information on the natural dynamics of the system to navigate around the family of equilibrium points in a controlled way.
54#
發(fā)表于 2025-3-30 21:46:37 | 只看該作者
John N. Williams,Eric W. K. Tsange vehicle has to glide at low Mach to reach the point close to the runway where automatic approach and landing starts. The algorithm presented here is based on the concept of Energy Corridor management and it is composed of two main elements: a trajectory propagator and a ground track generator. Imp
55#
發(fā)表于 2025-3-31 04:42:05 | 只看該作者
56#
發(fā)表于 2025-3-31 06:27:32 | 只看該作者
John N. Williams,Eric W. K. Tsangoptimal with respect to propellant usage, within a two-body problem context. If the conditions are not satisfied, one or more potential intermediate impulses are performed along the transfer arc, in order to lower the overall cost. The method is based on the propagation of the state transition matri
57#
發(fā)表于 2025-3-31 11:52:05 | 只看該作者
58#
發(fā)表于 2025-3-31 15:45:02 | 只看該作者
https://doi.org/10.1057/9781137509888ropellant. They can be used for missions studying astrophysics, heliophysics and planetary science. A formation flying system using solar radiation pressure is presented in this paper. The proposed formation flying mission uses sails due to the limited volume and power of small spacecraft. Station k
59#
發(fā)表于 2025-3-31 17:44:12 | 只看該作者
Katja Zolper,Daniel Beimborn,Tim Weitzeltudy both situations in the framework of a single, coherent model, the Hill restricted four-body problem. This model is presented in a Sun–Earth rotating reference frame to complement its earlier Earth–Moon frame formulation. We provide an overview of the planar quasi-periodic orbits that originate
60#
發(fā)表于 2025-4-1 00:24:36 | 只看該作者
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