Classical and Modern gain estimation approach of PID controller for the pitch control of the RCTA aircraft
In the current age of globalization, the development of autopilots is superficial as the standard of living is improved through aerial surveillance, defense applications, and door- to-door transportation. To design the PID controller, a mathematical model is created to address the system identificat...
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| Hauptverfasser: | , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2022-03-01
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| Schriftenreihe: | INCAS Bulletin |
| Schlagworte: | |
| Online-Zugang: | https://bulletin.incas.ro/files/jaiswal-r__prakash-o__vol_14_iss_1.pdf |
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