| 发明名称 |
DIFFERENTIAL STEERING CONTROL OF ELECTRIC TAXI LANDING GEAR |
| 摘要 |
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. |
| 申请公布号 |
US2015375854(A1) |
申请公布日期 |
2015.12.31 |
| 申请号 |
US201414317112 |
申请日期 |
2014.06.27 |
| 申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
Abel Stephen;Lazarovich David;Nutaro Joseph |
| 分类号 |
B64C25/40;G05D1/00 |
主分类号 |
B64C25/40 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft taxi control system comprising:
a left main gear (MG) drive motor; a right MG drive motor; a first motor drive controller configured to produce a left motor torque application signal responsively to nose gear angle (NGA) and nose wheel speed (NGS); and a second motor drive controller configured to produce a right motor torque application signal responsively to the NGA and the NGS, said left motor torque application signal and said right motor torque application signal being coordinated to reduce lateral loading of a nose wheel during a turning maneuver. |
| 地址 |
Morristown NJ US |
