Integration of Luenberger estimator with control reconfiguration system for hypersonic aircraft

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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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Bibliographic Details
Main Author:	Zaludin, Zairil
Format:	Conference or Workshop Item
Published:	IEEE 2023
Online Access:	http://psasir.upm.edu.my/id/eprint/37134/

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