An aircraft taxi control system may include a left main gear (MG) drive motor, a right MG motor, a first motor drive controller configured to produce a left motor torque signal responsively to nose gear angle (NGA) and nose wheel speed (NGS), and a second motor drive controller configured to produce a right motor toque signal responsively to the NGA and the NGS. The left motor torque signal and the right motor torque signal may be coordinated to reduce lateral loading of the nose wheel during a turning maneuver.
DIFFERENTIAL STEERING CONTROL OF ELECTRIC TAXI LANDING GEAR
2015-12-31
Patent
Electronic Resource
English
Landing Gear (Engine Off) Taxi System
SAE Technical Papers | 2021
Adaptive Landing Gear for Improved Taxi Performance
NTIS | 1977
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