Terminal control of the trajectory and rotational motion of an active spacecraft during a rendezvous with a passive spacecraft
- 作者: Zubov N.1,2, Mikrin E.1,2, Oleinik A.1,2, Ryabchenko V.1,2
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隶属关系:
- Bauman State Technical University
- OAO RKK Energiya
- 期: 卷 55, 编号 3 (2016)
- 页面: 435-445
- 栏目: Control Systems of Moving Objects
- URL: https://journals.rcsi.science/1064-2307/article/view/219646
- DOI: https://doi.org/10.1134/S1064230716030187
- ID: 219646
如何引用文章
详细
In this work, the problem of a spacecraft’s rendezvous is considered in the radial coordinate system, taking into consideration the effect of the difference gravitational acceleration, using a control algorithm with the prediction model based on the minimization of the generalized work functional. The analytical formulas have been derived to compute the control actions when the motion of the center of mass and the motion about the center of mass, when solving the parametric optimization problem, are considered in a unified terminal formulation. The analytical solution is based on a special prediction model that has an analytical solution in the advanced modeling of the rendezvous process. The results of modeling a spacecraft’s rendezvous are presented.
作者简介
N. Zubov
Bauman State Technical University; OAO RKK Energiya
编辑信件的主要联系方式.
Email: nik.zubov@gmail.com
俄罗斯联邦, Moscow, 105005; Korolev, Moscow oblast, 141070
E. Mikrin
Bauman State Technical University; OAO RKK Energiya
Email: nik.zubov@gmail.com
俄罗斯联邦, Moscow, 105005; Korolev, Moscow oblast, 141070
A. Oleinik
Bauman State Technical University; OAO RKK Energiya
Email: nik.zubov@gmail.com
俄罗斯联邦, Moscow, 105005; Korolev, Moscow oblast, 141070
V. Ryabchenko
Bauman State Technical University; OAO RKK Energiya
Email: nik.zubov@gmail.com
俄罗斯联邦, Moscow, 105005; Korolev, Moscow oblast, 141070
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