Design and verification of carefree maneuvering protection for a high performance fighter aircraft
Flight envelope protection for a high-performance aircraft poses a challenge to the designers and involves a time-consuming procedure to verify the protection. This paper presents a design approach to protect the aircraft from departure by a command path limiter for a rate command attitude hold cont...
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| Main Authors: | , , |
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| 其他作者: | |
| 格式: | Article |
| 語言: | English |
| 出版: |
2024
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| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/173978 |
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