Robust Control of a Gyroscopic Stabilizer at Sliding Modes
- Authors: Meshchanov A.S.1, Gataullina L.A.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 4 (2018)
- Pages: 671-676
- Section: 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
Cite item
Abstract
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.
About the authors
A. S. Meshchanov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: mas41@list.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111
L. A. Gataullina
Tupolev Kazan National Research Technical University
Email: mas41@list.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111