YAW REDUCTION SYSTEM AND METHOD FOR AIRCRAFT BRAKING

An aircraft brake control system accommodates desired yaw for steering, while substantially eliminating undesired yaw. The system assesses brake command signals from the pilot, signals corresponding to aircraft parameters, and signals based on brake control parameters, and determines therefrom an am...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: HILL, JAMES L, BURKHALTER, KURT, ROE, DAVID N, QUICKFALL, BENJAMIN ROBERT PIERCY
Format: Patent
Sprache:eng ; fre
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