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...
| Main Authors: | , , |
|---|---|
| Other Authors: | |
| Format: | Journal Article |
| Language: | English |
| Published: |
2024
|
| Subjects: | |
| Online Access: | https://hdl.handle.net/10356/173978 |