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...
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| Format: | Conference or Workshop Item |
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IEEE
2023
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| Online Access: | http://psasir.upm.edu.my/id/eprint/37134/ https://ieeexplore.ieee.org/document/10193439 |
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