Autonomous navigation during the final ascent of a spacecraft into the geostationary orbit. II. Simulation of operation of an integrated autonomous SC navigation and control system
- 作者: Voiskovskii A.1, Kozorez D.1, Krasil’shchikov M.1, Kruzhkov D.1, Sypalo K.2
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隶属关系:
- Moscow Aviation Institute
- Central Aerohydrodynamic Institute
- 期: 卷 55, 编号 5 (2016)
- 页面: 785-795
- 栏目: Navigation Systems
- URL: https://journals.rcsi.science/1064-2307/article/view/219729
- DOI: https://doi.org/10.1134/S1064230716050130
- ID: 219729
如何引用文章
详细
This study continues the series of papers devoted to the approach to solving the problem of autonomous navigation of a spacecraft (SC) in a geostationary orbit at all stages of its lifecycle: final ascent, transfer to the operating longitude, remaining at the operating longitude, removal from the orbit, and burial. In [1], we formulated the concept of autonomous navigation of a spacecraft at the stage of its final ascent to a geostationary orbit. This stage is most complicated from the technical point of view, taking into account the nonlinearity of the applied mathematical models, the influence of uncontrollable factors of various physical nature, and the necessity of the application of promising hardware (electric low-thrust engine, onboard receiver of signals from global navigation satellite systems, intersatellite communication channels, etc.). Taking this into account, the only constructive method for proving the viability and efficiency (taking into account the requirements formulated by the customer who placed the order) of the developed concept of the autonomous navigation at the final ascent stage in the mathematical simulation of this process. The subject of this study is to demonstrate the capabilities of the developed concept of autonomous navigation from the point of view of achieving the required level of reliability and accuracy in solving the navigation problem at the final ascent stage. This demonstration is based on the analysis of the results of imitating the simulation of the process of a spacecraft’s final ascent to a geostationary orbit obtained using the specially developed software complex.
作者简介
A. Voiskovskii
Moscow Aviation Institute
Email: kruzhkovd@mail.ru
俄罗斯联邦, Moscow
D. Kozorez
Moscow Aviation Institute
Email: kruzhkovd@mail.ru
俄罗斯联邦, Moscow
M. Krasil’shchikov
Moscow Aviation Institute
Email: kruzhkovd@mail.ru
俄罗斯联邦, Moscow
D. Kruzhkov
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: kruzhkovd@mail.ru
俄罗斯联邦, Moscow
K. Sypalo
Central Aerohydrodynamic Institute
Email: kruzhkovd@mail.ru
俄罗斯联邦, Moscow
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