Systems and aircraft are provided. An avionics system for an aircraft includes: a trajectory selection module configured to select a potential aircraft path relative to a current aircraft flight condition; a trajectory flight condition module configured to estimate a modeled flight condition of the aircraft along the potential aircraft path; a limit comparison module configured to determine whether the modeled flight condition violates aircraft limits; and a violation indicator module configured to generate an indication of impending violation.
AIRCRAFT FLIGHT ENVELOPE PROTECTION AND RECOVERY AUTOPILOT
SCHUTZ DER FLUGBEREICHSGRENZE FÜR FLUGZEUGE UND WIEDERHERSTELLUNGSAUTOPILOT
PROTECTION D'ENVELOPPE DE VOL D'AÉRONEF ET PILOTE AUTOMATIQUE DE RÉCUPÉRATION
2020-02-05
Patent
Electronic Resource
English
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