A flight control law enhances braking efficiency through the operation of aircraft elevators (or another pitch control system) using measured longitudinal acceleration and/or pedal position as references to the control law. Through this solution, it is possible to increase the vertical load in the main landing gear and consequently enhance braking efficiency.
USE OF AUTOMATIC PITCH CONTROL TO IMPROVE BRAKING PERFORMANCE
VERWENDUNG EINER AUTOMATISCHEN NICKSTEUERUNG ZUR VERBESSERUNG DER BREMSLEISTUNG
UTILISATION DE COMMANDE AUTOMATIQUE DE TANGUAGE POUR AMÉLIORER LA PERFORMANCE DE FREINAGE
2020-01-01
Patent
Elektronische Ressource
Englisch
USE OF AUTOMATIC PITCH CONTROL TO IMPROVE BRAKING PERFORMANCE
Europäisches Patentamt | 2018
|Use of automatic pitch control to improve braking performance
Europäisches Patentamt | 2018
|SAE Technical Papers | 2007
|British Library Conference Proceedings | 2007
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