THE DYNAMICS CONTROL OF THE RIGID WING UAV BY THE EXAMPLE OF USING LQR, LQG AND NONLINEAR CONTROL METHODS
Small - sized fixed-wing unmanned aerial vehicles (UAVs) have become a popular research topic in recent years.
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| Main Authors: | , |
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| Format: | Article |
| Language: | Russian |
| Published: |
North-Caucasus Federal University
2022-08-01
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| Series: | Современная наука и инновации |
| Subjects: | |
| Online Access: | https://msi.elpub.ru/jour/article/view/83 |
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