Integration of Luenberger estimator with control reconfiguration system for hypersonic aircraft
Dynamic instability of hypersonic aircraft was well known. To ensure a stable and controlled flight throughout the hypersonic flight phase, a robust automatic flight control system was needed. In addition, in the unlikely event of a flight control failure, the autopilot must be able to remain operat...
| Main Author: | |
|---|---|
| Format: | Conference or Workshop Item |
| Published: |
IEEE
2023
|
| Online Access: | http://psasir.upm.edu.my/id/eprint/37134/ |