| Autor: |
Karimtaevna, Satybaldina Dana, Bekbolatovna, Amirzhanova Zinara, Assilkhanovna, Mashtayeva Aida |
| Předmět: |
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| Zdroj: |
International Journal of Electrical & Computer Engineering (2088-8708); Aug2022, Vol. 12 Issue 4, p3572-3582, 11p |
| Abstrakt: |
One of the most dangerous parts of the flight is the landing phase, as most accidents occur at this stage. In order to reduce the effect of the low-level wind shear on the longitudinal motion of the aircraft in the glide path landing mode (task) a robust H- control isproposed. Dynamic models of the plane and wind shear are built. 2 and 8 synthesis methods are investigated for the task of aircraft flight control in a vertical plane during landing under conditions of undefined disturbances. Both control methods allow to reduce height deviation significantly. However, suboptimal control 8 provides better quality of transition processes both in height and speed than optimal control 2. The results of simulation of the synthesized system confirm the effectiveness of 8 - control for increasing robust stability to uncertainties caused by wind disturbances. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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