Steep approach performance improvements and optimization

A flight control system can achieve a relatively steep descent (using drag devices such as flight spoilers) at relatively low speeds while retaining good airplane handling qualities from the pilot's point of view. The system and method optimize the drag device's positioning used to perform...

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Bibliographic Details
Main Authors CALDEIRA FABRICIO REIS, OLIVEIRA MAURICIO FAUSTINO, DE TARSO FERREIRA DANIEL PAULO
Format Patent
LanguageEnglish
Published 06.10.2015
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Summary:A flight control system can achieve a relatively steep descent (using drag devices such as flight spoilers) at relatively low speeds while retaining good airplane handling qualities from the pilot's point of view. The system and method optimize the drag device's positioning used to perform steep approach to improve performance.
Bibliography:Application Number: US201314096777