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樓主
發(fā)表于 2025-3-21 19:26:01 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Guidance and Control Technology of Spacecraft on Elliptical Orbit
編輯Fucheng Liu,Shan Lu,Yue Sun
視頻videohttp://file.papertrans.cn/391/390762/390762.mp4
叢書名稱Navigation: Science and Technology
圖書封面Titlebook: ;
出版日期Book 2019
版次1
doihttps://doi.org/10.1007/978-981-10-7959-7
isbn_softcover978-981-13-4028-4
isbn_ebook978-981-10-7959-7Series ISSN 2522-0454 Series E-ISSN 2522-0462
issn_series 2522-0454
The information of publication is updating

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沙發(fā)
發(fā)表于 2025-3-21 21:26:19 | 只看該作者
https://doi.org/10.1007/978-1-4419-9946-7 orbit, which the spacecraft is on is not zero, and the point with the smallest distance from spacecraft operating under this condition to the earth is called perigee, and the farthest point is called apogee.
板凳
發(fā)表于 2025-3-22 02:26:51 | 只看該作者
https://doi.org/10.1007/0-387-32845-9he single spacecraft. In this chapter, we will introduce the orbit design method of the multi-spacecraft formation in the elliptical orbit, that is, the relative configuration design method of the formation flight.
地板
發(fā)表于 2025-3-22 05:27:49 | 只看該作者
5#
發(fā)表于 2025-3-22 11:13:36 | 只看該作者
https://doi.org/10.1007/978-981-10-5550-8tion system and autonomous measuring equipments onboard to get information without relying on ground station measurement and control and combines it with the orbit prediction information of high accuracy; then, long-term high-precision orbit parameters of the whole constellation will be obtained by
6#
發(fā)表于 2025-3-22 16:51:39 | 只看該作者
Markov Model and Hidden Stochastic Modelanghai (02):45–54 [.], Yang et al. in Aerosp Shanghai 27(2):38–45 [.], Shi et al. in Aerosp Control 28(6):43–48 [.]) by using spaceborne measuring equipment and combining with the relative motion equation and state estimation method of spacecraft.
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發(fā)表于 2025-3-22 17:18:29 | 只看該作者
8#
發(fā)表于 2025-3-22 22:25:03 | 只看該作者
Formation Configuration Design of Elliptical Orbit,he single spacecraft. In this chapter, we will introduce the orbit design method of the multi-spacecraft formation in the elliptical orbit, that is, the relative configuration design method of the formation flight.
9#
發(fā)表于 2025-3-23 04:31:03 | 只看該作者
10#
發(fā)表于 2025-3-23 09:26:24 | 只看該作者
Autonomous Navigation Technology of Regional Constellation,tion system and autonomous measuring equipments onboard to get information without relying on ground station measurement and control and combines it with the orbit prediction information of high accuracy; then, long-term high-precision orbit parameters of the whole constellation will be obtained by
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