Analytical Synthesis of a Modal Controller by Output Vector for Attitude Control of a Descent Module during Its Descent in the Earth’s Atmosphere
- 作者: Zubov N.E.1, Lapin A.V.1, Ryabchenko V.N.1
-
隶属关系:
- Bauman Moscow State Technical University
- 期: 卷 62, 编号 3 (2019)
- 页面: 401-416
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/231028
- DOI: https://doi.org/10.3103/S1068799819030073
- ID: 231028
如何引用文章
详细
A new analytical algorithm of modal control is developed for the sixth-order control system that represents the problem of descent module attitude stabilization using the values of two angles measured by free gyroscope and three components of angular velocity vector with respect to the corresponding coordinate axes measured by the angular velocity sensor. This algorithm belongs to the category of dynamic object control algorithms by the output vector and it is based on synthesis of a state vector observer.
作者简介
N. Zubov
Bauman Moscow State Technical University
编辑信件的主要联系方式.
Email: nezubov@bmstu.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
A. Lapin
Bauman Moscow State Technical University
Email: nezubov@bmstu.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
V. Ryabchenko
Bauman Moscow State Technical University
Email: nezubov@bmstu.ru
俄罗斯联邦, ul. 2-ya Baumanskaya 5, Moscow, 105005
补充文件
