Linear dynamic mathematical model and identification of micro turbojet engine for Turbofan Power Ratio control
Micro turbojets can be used for propulsion of civilian and military aircraft, consequently their investigation and control is essential. Although these power plants exhibit nonlinear behaviour, their control can be based on linearized mathematical models in a narrow neighbourhood of a selected oper...
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2019-12-01
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| Series: | Aviation |
| Subjects: | |
| Online Access: | https://journals.vgtu.lt/index.php/Aviation/article/view/11653 |