Robust Control of a Gyroscopic Stabilizer at Sliding Modes
- 作者: Meshchanov A.S.1, Gataullina L.A.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 4 (2018)
- 页面: 671-676
- 栏目: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230772
- DOI: https://doi.org/10.3103/S1068799818040268
- ID: 230772
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详细
The method is obtained for the optical device axis stabilization by pitch and yaw angles at sliding modes in the conditions of nonlinearity, unsteadiness, cross-coupled and non-invariance to uncertainties. The quality of transients is formed by rotations and displacements of two sliding planes relative to the origin. Accuracy is achieved by adjusting the control parameters and reducing uncertainty with increasing accuracy of its identification and compensation.
作者简介
A. Meshchanov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
L. Gataullina
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111
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